Author Topic: LIVE: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (11:20 UTC)  (Read 69211 times)

Offline ss1_3

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Thread for the next GSLV MkII flight carrying INSAT 3DR- replacement for the INSAT 3D satellite (meteorological).

http://www.newindianexpress.com/states/kerala/Next-GSLV-Mission-in-July-2016-VSSC/2015/08/30/article3000786.ece

Quote
The next Geosynchronous Satellite Launch Vehicle launch will be the GSLV F09 mission and we plan to have it in July 2016
.
.
The GSLV F09 mission will have any one of the three satellites - GSAT-9, GSAT-7A or the INSAT 3DR - as payload, depending on the priority at the time

Relevant Links:

https://en.wikipedia.org/wiki/INSAT-3D
http://www.wmo-sat.info/oscar/satellites/view/194
http://space.skyrocket.de/doc_sdat/insat-3d.htm
« Last Edit: 09/08/2016 12:38 pm by Satori »

Offline ss1_3

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Re: GSLV F09, INSAT 3DR, SLP, NET Jul 2016
« Reply #1 on: 12/17/2015 07:12 am »
INSAT- 3DR payload flagged off


 After Successful Test & Evaluation, INSAT-3DR Payload (Sounder & Imager) was delivered to ISITE/ISAC on November 19, 2015.


Offline m.prasad

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Re: GSLV F09, INSAT 3DR, SLP, NET Jul 2016
« Reply #2 on: 12/17/2015 12:37 pm »
Why ISRO has selected INSAT-3DR over other satellites as already INSAT-3D in orbit with the same Imager & Sounder?

Does any one have idea on this?

Thx
~Prasad

Offline Ohsin

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Re: GSLV F09, INSAT 3DR, SLP, NET Jul 2016
« Reply #3 on: 12/17/2015 02:29 pm »
FYI this should be the first launch where the indigenous cryo is flown in uprated configuration. Thrust will be increased from 73.55kn to 93.1kn and propellent loading will be increased from 12.8 tons to 15 tons.

Can you point me to source on that :)

Also from http://www.isro.gov.in/update/03-sep-2015/gslv-saga

Quote
The next mission, designated as GSLV-F05, is targeted for launch in July 2016 and will carry the 2200 kg INSAT-3DR meteorological satellite.  GSLV-F09 is planned in May 2017 to launch the GSAT-9 satellite.
"Well, three cheers to Sharma, but our real baby is INSAT."

Offline Ohsin

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Re: GSLV F09, INSAT 3DR, SLP, August 2016
« Reply #4 on: 03/31/2016 02:06 pm »
Quote
INSAT-3DR Communication Payload Flag off

After Successful Test & Evaluation, INSAT-3DR Payload was dispatched to ISITE/ISAC on March 16, 2016.

Attached PDF has some INSAT 3DR information
« Last Edit: 03/31/2016 02:20 pm by Ohsin »
"Well, three cheers to Sharma, but our real baby is INSAT."

Offline tehwkd

Re: GSLV F09, INSAT 3DR, SLP, August 2016
« Reply #5 on: 05/01/2016 05:41 am »
Article mentions dual payload with one being the INSAT-3DR, doesn't mention the name of the other

http://www.newindianexpress.com/cities/chennai/ISRO-to-Launch-Two-New-Meteorological-Satellites/2016/05/01/article3409349.ece
Custodian of NextLaunch & LaunchStuff |   Utilizer of Google

Offline vineethgk

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Re: GSLV F09, INSAT 3DR, SLP, August 2016
« Reply #6 on: 05/01/2016 05:55 am »
Article mentions dual payload with one being the INSAT-3DR, doesn't mention the name of the other

http://www.newindianexpress.com/cities/chennai/ISRO-to-Launch-Two-New-Meteorological-Satellites/2016/05/01/article3409349.ece
The second meteorological payload should be referring to SCATSAT, which is planned to be launched in a PSLV flight later this year.

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Offline vyoma

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Re: GSLV F09, INSAT 3DR, SLP, August 2016
« Reply #7 on: 05/27/2016 11:58 pm »
INSAT 3DR will be launched by GSLV-Mk2 F05 as per ISOR 2015-16 annual report.

Quote
The realisation of subsystems/stages for the next flight GSLV-F05 has commenced. GSLV-F05 carrying INSAT-3DR satellite, is targeted for launch during the third quarter of 2016.
« Last Edit: 05/27/2016 11:59 pm by vyoma »

Offline vyoma

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Re: GSLV F09, INSAT 3DR, SLP, August 2016
« Reply #8 on: 07/23/2016 01:00 am »
http://gadgets.ndtv.com/science/news/isro-to-launch-insat-3dr-weather-satellite-in-august-864096

Quote
The Indian Space Research Organisation (Isro) will launch INSAT-3DR next month with its GSLV rocket, said Kiran Kumar at the Madras Institute of Technology Alumni Association meeting in Chennai.

Offline input~2

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Re: GSLV F09, INSAT 3DR, SLP, mid September 2016
« Reply #9 on: 07/23/2016 07:37 am »
already slipped to 2nd week of September
http://www.andhrabhoomi.net/content/nation-829

Offline vineethgk

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Re: GSLV F05, INSAT 3DR, SLP, mid-September 2016
« Reply #10 on: 07/29/2016 12:46 pm »
Isro Looking to Launch INSAT-3DR Weather Satellite on August 28

Quote
Preparations for the launch of weather satellite INSAT-3DR with the geosynchronous satellite launch vehicle (GSLV-MkII) next month are progressing at Sriharikota, officials said on Friday.
"The weather satellite INSAT-3DR will be put into orbit by a GSLV rocket August end. Preparations for the launch are going on," P. Kunhi Krishnan, Director of the Satish Dhawan Space Centre (SDSC), told IANS.

It is learnt that the launch is tentatively slated for August 28.

Offline vineethgk

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Re: GSLV F05, INSAT 3DR, SLP, August 28 2016
« Reply #11 on: 08/04/2016 09:25 pm »
Indian GSLV will truly ‘arrive’ this month

Quote
Enters the all-Indian GSLV, finally, later this month. The GSLV-F05 flight coming up on August 28 or 29 will be its first regular, full-service or 'operational' one
Quote
GSLV-Mk2 however can put only satellites weighing up to 2,200 kg into geostationary space. At least four more of them are in the making now.
Quote
Another official said the plan is to do two GSLV launches a year from next year, apart from doubling the PSLV rate to ten or a dozen a year.

Offline input~2

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Re: GSLV F05, INSAT 3DR, SLP, August 29 2016
« Reply #12 on: 08/07/2016 02:37 pm »
Launch now announced for August 29 at 11:00 UTC
Satellite launch mass: 2061 kg
source

Offline worldtimedate

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Re: GSLV F05, INSAT 3DR, SLP, August 29 2016
« Reply #13 on: 08/08/2016 06:50 am »
Launch now announced for August 29 at 11:00 UTC
Satellite launch mass: 2061 kg
source

INSAT 3DR weighing only 2061 seems to be little lighter than it should be. Last year GSLV launched a satellite GSAT-6 weighing 2117kg. GSLV Project Manager Umamaheshwaran said last year after the launch that his team would gradually increase the payload up to maximum 2.5 ton by tweaking cryogenic engine in the subsequent launches.

Bur right now, it seems that GSLV II can't go beyond 2.2 ton capacity.

Quote
GSLV-Mk2 however can put only satellites weighing up to 2,200 kg into geostationary space. At least four more of them are in the making now.
source

Source :
Indian GSLV will truly ‘arrive’ this month

--- [ --- ]
« Last Edit: 08/08/2016 07:02 am by worldtimedate »

Offline sportyfailure

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Re: GSLV F05, INSAT 3DR, SLP, August 29 2016
« Reply #14 on: 08/11/2016 12:41 pm »
Article noticed By Ohsin and trasnslated by me

A pyrocutter in the solar panel deployment mechanism was found to be faulty and needs to be replaced. Launch may be delayed by 3 days or 1 week.


ఇన్సాట్‌-3డీఆర్‌ ఉపగ్రహంలో సాంకేతిక లోపం
జీఎస్‌ఎల్‌వీ ప్రయోగం వాయిదా పడే అవకాశం
శ్రీహరికోట, న్యూస్‌టుడే: శ్రీపొట్టి శ్రీరాములు నెల్లూరు జిల్లాలోని సతీశ్‌ ధవన్‌ అంతరిక్ష కేంద్రం షార్‌ (శ్రీహరికోట) నుంచి ఈ నెల 29న నింగిలోకి పంపాల్సిన జియోసింక్రనస్‌ శాటిలైట్‌ లాంచ్‌ వెహికల్‌ (జీఎస్‌ఎల్‌వీ) ప్రయోగం వాయిదా పడనుందని సమాచారం. జీఎస్‌ఎల్‌వీ ద్వారా 2,200 కిలోల బరువున్న ఇన్సాట్‌-3డీఆర్‌ ఉపగ్రహాన్ని నిర్ణీత కక్ష్యలోకి ప్రవేశ పెట్టాల్సి ఉంది. రాకెట్‌లో ఉపగ్రహాన్ని అనుసంధానం చేసే ముందు పరీక్షలు నిర్వహిస్తున్నారు. అయితే ఉపగ్రహంలోని సోలార్‌ ప్యానల్‌ పని చేసేందుకు అమర్చిన ‘పైరోకట్టర్‌’ పనితీరు అంచనాలను అందుకోలేదని తాజాగా గుర్తించినట్లు సమాచారం. దీంతో పైరోకట్టర్‌ను మార్చాలని శాస్త్రవేత్తలు నిర్ధారణకు వచ్చారు. పాత పైరోకట్టర్లు శాస్త్రవేత్తలకు అందుబాటులో ఉన్నాయి. వీటిలో ఒకదానిని సోలార్‌ ప్యానల్‌కు అమర్చితే సరిపోతుందా? లేక.. కొత్తదానిని తయారు చేసి అమర్చాలా.. అనే విషయంలో శాస్త్రవేత్తలు సందిగ్ధంలో ఉన్నారు. అందుబాటులో ఉన్న పైరోకట్టర్‌ను సోలార్‌ ప్యానల్‌కు అమర్చే నేపథ్యంలో జీఎస్‌ఎల్‌వీ ప్రయోగం మూడు రోజులు, కొత్తదానినే అమర్చాలంటే వారానికిపైగా వాయిదా పడే అవకాశం ఉంది.
ఎంఆర్‌ఆర్‌లో ఖరారు కాని ప్రయోగ తేదీ
షార్‌లోని బ్రహ్మప్రకాష్‌ హాలులో బుధవారం ఉదయం నుంచి సాయంత్రం వరకు జీఎస్‌ఎల్‌వీకి సంబంధించిన రాకెట్‌ సన్నద్ధత సమావేశం (ఎంఆర్‌ఆర్‌) జరిగింది. ఉపగ్రహంలోని సోలార్‌ ప్యానల్‌లో వచ్చిన లోపాలపై సుధీర్ఘంగా చర్చించారు. ఈ నేపథ్యంలో రాకెట్‌ ప్రయోగ తేదీని ఖరారు చేయలేదని తెలిసింది. ఈ విషయమై మళ్లీ గురువారం సమావేశం కావాలని శాస్త్రవేత్తలు నిర్ణయించారు
http://www.eenadu.net/news/news.aspx?item=ap-main-news&no=15
Translation by /u/standardengineer
INSAT-3DR satellite has a technical issue.
GSLV launch likely to be delayed.
SHAR: As per sources GSLV launch due for Aug 29 is likely to be delayed. Launcher-satellite integration tests are going on. A pyrocutter is used to deploy solar panels in the satellites. The pyrocutter on INSAT-3DR did not meet the standards. They have decided to replace the pyrocutter. Spares are available. Scientists are studying whether to use a spare or to make a new one. GSLV launch will be delayed by three days if they use a spare pyrocutter, it could be delayed by a week if they decide to use a new pyrocutter.
Launch date was not agreed upon in the MRR.
MRR occured at Wednesday evening. They discussed the problems noticed in the solar panels. For this reason launch date was not confirmed. another review meet will happen on thursday.
Tl;DR; A pyrocutter used to deploy solar panels was found to be faulty and will need to be replaced.

Offline input~2

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Re: GSLV F05, INSAT 3DR, SLP, September 2016
« Reply #15 on: 08/11/2016 07:17 pm »
Also here an indication that Insat 3DR will now be launched in September
http://www.goinews.com/2016/08/08/isro-launch-2-new-meteorological-satellites-september/

Offline input~2

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Re: GSLV F05, INSAT 3DR, SLP, NET September 8 2016
« Reply #16 on: 08/14/2016 02:29 pm »
Launch postponed 10 days, so NET September 8
source

Offline input~2

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Re: GSLV F05, INSAT 3DR, SLP, September 10 2016
« Reply #17 on: 08/16/2016 04:25 pm »
Launch now planned for September 10
Source

Offline vyoma

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Re: GSLV F05, INSAT 3DR, SLP, September 10 2016
« Reply #18 on: 08/16/2016 06:55 pm »
http://www.deccanchronicle.com/science/science/160816/new-gslv-launch-in-september.html

Quote
Scientists of the Indian Space Research Organisation (Isro) have been gearing up for the launch of the Geo-synchronous Satellite Launch Vehicle (GSLV-F05) carrying 2,200 kg of meteorological satellite INSAT-3DR on board most likely on September 10 this year. This is one among the four rocket launches planned by Isro before the end of this year.

Offline input~2

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Re: GSLV F05, INSAT 3DR, SLP, September 8 2016
« Reply #19 on: 08/25/2016 09:30 am »
Launch now planned for September 8
source

Offline input~2

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Re: GSLV F05, INSAT 3DR, SLP, September 8 2016
« Reply #20 on: 08/27/2016 08:39 am »
Planned launch time seems to be 11:22 UTC (04:52 pm IST)
http://www.andhrabhoomi.net/content/state-3945

Offline vyoma

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Re: GSLV F05, INSAT 3DR, SLP, September 8 2016
« Reply #21 on: 08/27/2016 07:47 pm »
http://www.ndtv.com/india-news/isro-to-test-scramjet-engine-on-sunday-1451043

Quote
Earlier Mr Krishnan had said the Indian weather satellite will be launched on August 28 which has now been postponed to September 8.

Queried about the change in launch plan Krishnan said: "While carrying out the tests there was a technical issue found with a satellite component. It has been sorted out now and hence the delay."

He said the GSLV rocket that would carry the weather satellite INSAT-3DR is fully assembled.

The weather satellite will be mounted on to the rocket in three to four days.

Offline worldtimedate

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Re: GSLV F05, INSAT 3DR, SLP, September 8 2016
« Reply #22 on: 08/30/2016 07:37 pm »
Quote

THIRUVANANTHAPURAM: Buoyed by the success of the ISRO's Sramjet engine test on Sunday, Scientists of Vikram Sarabhai Space Centre (VSSC) and Liquid Propulsion Systems Centre (LPSC) have begun preparations for the launch of GSLV Mark II scheduled for Sep 8.

"Now, the preparations are on for the GSLV Mark II mission on Sept 8 for the launch of INSAT-3DR, an Indian satellite for weather forecast, search and rescue information. It will be the second flight using the indigenously developed cryogenic engine after it was successfully used for the first time to launch GSLV-D5 in 2014," VSSC director K Sivan told TOI.

The indigenous cryogenic engine to be used for GSLV Mark II on Sept 8 will be similar to the one used in GSLV-D5 launch two years back, the scientists said.


Source :
Preparations on for launch of GSLV Mark II

--- [ --- ]
« Last Edit: 08/30/2016 07:40 pm by worldtimedate »

Offline Ohsin

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Re: GSLV F05, INSAT 3DR, SLP, September 8 2016
« Reply #23 on: 09/01/2016 06:22 pm »
Quote
Sep 01, 2016
GSLV-F05 / INSAT-3DR Mission is scheduled to be launched on Sept 08, 2016 at 16:10 hrs (IST) from SDSC, SHAR, Sriharikota
« Last Edit: 09/01/2016 06:28 pm by Ohsin »
"Well, three cheers to Sharma, but our real baby is INSAT."

Offline worldtimedate

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Re: GSLV F05, INSAT 3DR, SLP, September 8 2016
« Reply #24 on: 09/01/2016 07:43 pm »
There were conflicting reports in many newspapers about if INSAT 3DR is a 2061 Kg or 2200 Kg Satellite.
But all the misinformation is laid to rest by the ISRO Website INSAT 3DR page.

It is a 2211 Kg Satellite, an increase of odd 100 kg than the satellite launched by GSLV MK II last year.

[/quote]

INSAT-3DR has a lift-off mass of 2211 kg, which includes about 1255 kg of propellant. The propellant carried by INSAT-3DR is mainly required to raise the satellite from the Geosynchronous Transfer Orbit (GTO) to its final Geostationary Orbit and to maintain the satellite in its orbital slot during its life. INSAT-3DR is based on ISRO's two Tonne Class platform (I-2K bus) employing light-weight structural elements like Carbon Fibre Reinforced Plastic (CFRP). The satellite has a solar array generating 1700 Watts of power.

GSLV-F05 / INSAT-3DR Mission is scheduled to be launched on Sept 08, 2016 at 16:10 hrs (IST) from SDSC, SHAR, Sriharikota.

[/quote]

Source :
INSAT-3DR

--- [ --- ]

Offline Ohsin

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #25 on: 09/02/2016 08:18 am »
Brochure is out.
"Well, three cheers to Sharma, but our real baby is INSAT."

Offline Ohsin

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #26 on: 09/02/2016 11:49 am »
On its way  ;D
"Well, three cheers to Sharma, but our real baby is INSAT."

Offline isro-watch

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #27 on: 09/02/2016 12:57 pm »
Is there any specific reason why the GSLV is moved to the pad a full 5-6 days before the launch ?

Offline vineethgk

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #28 on: 09/02/2016 01:19 pm »
Is there any specific reason why the GSLV is moved to the pad a full 5-6 days before the launch ?
Isn't that the usual time frame, approx?

EDIT: Feeling a bit jittery though, in light of the SpaceX incident yesterday.. Space is hard...
« Last Edit: 09/02/2016 01:24 pm by vineethgk »

Offline Stan Black

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #29 on: 09/02/2016 07:01 pm »
On its way  ;D

I see it is pedestal I.

Offline kanaka

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Re: GSLV F05, INSAT 3DR, SLP, September 8 2016
« Reply #30 on: 09/03/2016 02:00 am »
There were conflicting reports in many newspapers about if INSAT 3DR is a 2061 Kg or 2200 Kg Satellite.
But all the misinformation is laid to rest by the ISRO Website INSAT 3DR page.

It is a 2211 Kg Satellite, an increase of odd 100 kg than the satellite launched by GSLV MK II last year.


INSAT-3DR has a lift-off mass of 2211 kg, which includes about 1255 kg of propellant. The propellant carried by INSAT-3DR is mainly required to raise the satellite from the Geosynchronous Transfer Orbit (GTO) to its final Geostationary Orbit and to maintain the satellite in its orbital slot during its life. INSAT-3DR is based on ISRO's two Tonne Class platform (I-2K bus) employing light-weight structural elements like Carbon Fibre Reinforced Plastic (CFRP). The satellite has a solar array generating 1700 Watts of power.

GSLV-F05 / INSAT-3DR Mission is scheduled to be launched on Sept 08, 2016 at 16:10 hrs (IST) from SDSC, SHAR, Sriharikota.

[/quote]

Source :
INSAT-3DR

--- [ --- ]
[/quote]


India should think alternative ways of propelling the satellite so as to reduce flight mass. Japan has utilized eon propulsion system. Indian too can think of in such direction for cruising the bird on space.

Offline Steven Pietrobon

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #31 on: 09/03/2016 05:49 am »
GSAT 4 launched in 2010 had ion propulsion, but it failed to reach orbit. ISRO is working on using ion propulsion for its future satellites.

http://www.business-standard.com/article/technology/isro-to-use-electric-propulsion-on-satellites-to-carry-more-transponders-116011000356_1.html
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #32 on: 09/03/2016 06:09 am »
Information about ISRO's ion thrusters can be found here: https://forum.nasaspaceflight.com/index.php?topic=33770.0

GSAT-19E would be having ion thrusters for satellite station keeping. It would be launched aboard LVM3-D1 by the end of this year.

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #33 on: 09/03/2016 01:48 pm »
There were conflicting reports in many newspapers about if INSAT 3DR is a 2061 Kg or 2200 Kg Satellite.
But all the misinformation is laid to rest by the ISRO Website INSAT 3DR page.

It is a 2211 Kg Satellite, an increase of odd 100 kg than the satellite launched by GSLV MK II last year.


It seems an increase of odd 100 kg payload capacity has an effect in vehicle's guidance error margin - targeted inclination of 20.61° for GSLV F5  Vs  19.3° inclination achieved by GSLV D5/GSAT-14 mission. If you see past GSLV missions you can clearly observe gradual increase of inclination with increase of vehicle's payload capacity .
« Last Edit: 09/03/2016 01:56 pm by c.hazra200 »

Offline sanjaykumar

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #34 on: 09/05/2016 10:09 pm »
http://www.isro.gov.in/update/05-sep-2016/mission-readiness-review-mrr-committee-and-launch-authorization-board-lab-have


Mission Readiness Review (MRR) committee and Launch Authorization Board (LAB) have cleared the 29 hr countdown starting at 11.10 hr IST on Wednsday,September 7, 2016 and the launch of GSLV-F05/INSAT-3DR Mission for Thursday , September 8, 2016 at 16.10 hr

Offline input~2

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #35 on: 09/06/2016 02:55 am »
A1866/16 -  GSLV-F05 ROCKET LAUNCH FROM SHAR RANGE, SRIHARIKOTA WILL TAKE PLACE AS PER FLW DETAILS. THE LAUNCH WILL BE ON ANY ONE OF THE DAY DURING THIS PERIOD. ACTUAL DATE OF LAUNCH WILL BE INTIMATED 24HRS IN ADVANCE THROUGH A SEPERATE NOTAM. LAUNCH PAD COORD: 13 43.2 N   080 13.8 E NO FLT IS PERMITTED OVER THE DNG ZONE. A. DANGER ZONE -1 IS A CIRCLE OF 10NM AROUND THE LAUNCHER B. DANGER ZONE -2 IS A RECTANGULAR AREA BOUNDED BY: 1150N 08515E 1235N 08525E 1215N 08625E 1130N 08615E C. DANGER ZONE -3 IS A RECTANGULAR AREA BOUNDED BY: 1035N 08915E 1115N 08925E 1100N 09005E 1020N 08955E D. DANGER ZONE -4 IS A RECTANGULAR AREA BOUNDED BY: 0750N 09515E 0930N 09515E 0930N 09605E 0750N 09605E ROUTES AFFECTED IN CHENNAI FIR ARE: N571, P761, N877, W20, A465, P762, L510, P628, L645, Q10, Q11, Q23, Q24, V3, V4, V9 ? V11 CLOSURE/ALTERNATE ROUTINGS: 1)    N571 NOT AVBL BTN DORAM AND BIKEN ALTN ROUTE: DORAM-DCT-MMV VOR-DCT AVGIR-DCT BIKEN-N571 (BIDIRECTIONAL) 2)    P761 NOT AVBL MMV VOR AND PPB VOR ALTN ROUTE: MMV VOR- DCT- AVGIR-DCT-BIKEN-DCT- PT B 0943N 08935E - DCT- PPB VOR (BIDIRECTIONAL) 3)    N877 NOT AVBL BTN LAGOG AND ORARA ALTN ROUTE: LAGOG-DCT-POINT Z 1200N 08951E-DCT-ORARA (BIDIRECTIONAL) 4)    W20 NOT AVBL BTN MMV VOR AND BODEL //PART 1 OF 2 PARTS//. BTN 1000-1400, 08 SEP 10:00 2016 UNTIL 26 SEP 14:00 2016. CREATED: 02 SEP 09:37 2016

Offline seshagirib

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #36 on: 09/06/2016 07:04 am »
http://www.isro.gov.in/update/05-sep-2016/mission-readiness-review-mrr-committee-and-launch-authorization-board-lab-have


Mission Readiness Review (MRR) committee and Launch Authorization Board (LAB) have cleared the 29 hr countdown starting at 11.10 hr IST on Wednsday,September 7, 2016 and the launch of GSLV-F05/INSAT-3DR Mission for Thursday , September 8, 2016 at 16.10 hr

IIRC , PSLV coutdown = 48 hrs.

Count down of GSLV (~29 hrs ) << PSLV count down (~48 hrs).

Is this because the GSLV has one less stage ?
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Offline seshagirib

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #37 on: 09/07/2016 06:35 am »
http://www.isro.gov.in/update/07-sep-2016/29-hr-countdown-operation-of-gslv-f05-insat-3dr-mission-has-started-1110-hr-ist


Quote
Sep 07, 2016    The 29 hr countdown operation of GSLV-F05/INSAT-3DR Mission has started at 11:10 hr IST on Wednesday, September 7, 2016


« Last Edit: 09/07/2016 06:38 am by seshagirib »
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Offline sanjaykumar

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #38 on: 09/07/2016 08:03 am »

http://www.isro.gov.in/update/07-sep-2016/preparations-second-stage-gs2-propellant-filling-operation-are-under-progress

Preparations for Second stage (GS2) propellant filling operation are under progress





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Offline sanjaykumar

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #40 on: 09/07/2016 02:37 pm »
http://isro.gov.in/launcher/gslv-f05-insat-3dr

Second Stage (GS2) N2O4 filling completed by 13:30 hr IST. Preparations for Second Stage (GS2) UH25 filling are under progress

Second Stage (GS2) UH25 filling under progress

Second Stage (GS2) UH25 filling completed by 17:40 hr IST


Offline russianhalo117

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Re: GSLV F05, INSAT 3DR, SLP, September 8, 2016 (10:40 UTC)
« Reply #41 on: 09/07/2016 06:34 pm »
http://www.isro.gov.in/update/05-sep-2016/mission-readiness-review-mrr-committee-and-launch-authorization-board-lab-have


Mission Readiness Review (MRR) committee and Launch Authorization Board (LAB) have cleared the 29 hr countdown starting at 11.10 hr IST on Wednsday,September 7, 2016 and the launch of GSLV-F05/INSAT-3DR Mission for Thursday , September 8, 2016 at 16.10 hr

IIRC , PSLV coutdown = 48 hrs.

Count down of GSLV (~29 hrs ) << PSLV count down (~48 hrs).

Is this because the GSLV has one less stage ?
partly do to GSLV being a newer launcher amongst other reasons

Online Chris Bergin

Just to check, this is the first GSLV since the GSAT-6 launch a year ago?

Oh and moved for live coverage.
« Last Edit: 09/07/2016 08:50 pm by Chris Bergin »
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Offline edkyle99

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Just to check, this is the first GSLV since the GSAT-6 launch a year ago?

Oh and moved for live coverage.
Yes.

Here are Gunter's and my GSLV logs.
http://space.skyrocket.de/doc_lau/gslv.htm
http://www.spacelaunchreport.com/gslv.html#gslvlog

 - Ed Kyle

Offline Stan Black

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Just to check, this is the first GSLV since the GSAT-6 launch a year ago?

Oh and moved for live coverage.
Yes.

Here are Gunter's and my GSLV logs.
http://space.skyrocket.de/doc_lau/gslv.htm
http://www.spacelaunchreport.com/gslv.html#gslvlog

 - Ed Kyle

There was also an attempt to launch a GSLV in August 2013:-

Quote
The launch attempt of GSLV-D5 on August 19, 2013, was aborted due to a leak observed in the UH25 fuel system of the Liquid Second Stage (GS2) during the final phase of the countdown at 1:30 hrs before lift-off (T0). The Failure analysis board (FAB) concluded that a crack, attributed to Stress Corrosion Cracking (SCC), in the parent metal region of UH25 tank (material: Aluminium alloy AA7020) was the cause for the leak during the preflight pressurization of tank at T0-1:47 hr. Based on the impact assessment of the UH25 spillage on the vehicle systems, the GSLV-D5 vehicle for the next mission was prepared with new stages of GS2, L40 and GS1 (including core base shroud, interstages IS1/2V and IS1/2M). The Cryo stage, Payload fairing, Equipment bay and the GSAT-14 spacecraft were preserved and reused.
http://www.vssc.gov.in/VSSC_V4/images/Launchers_Brochures/GSLV-D5GSAT-14MISSION.pdf

Offline sanjaykumar

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http://isro.gov.in/update/07-sep-2016/uh25-filling-four-l40-strap-stages-completed-2100hr-ist
UH25 filling into four L40 Strap-On Stages completed by 21:00hr IST

Offline William Graham

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There was also an attempt to launch a GSLV in August 2013:

That would normally be classed as a scrub rather than an unsuccessful launch attempt although as you quoted they changed most of the rocket before it successfully launched in January 2014.


If this launch is successful it will be the first time the GSLV has completed three consecutive launches without a failure.

Offline sanman

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I used to hope that GSLV would go on to become as successful a workhorse as PSLV - but now I just hope that ISRO moves past it and keeps on iteratively improving LVM3 to better and better platforms, like an HLV


Offline vyoma

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Quote
Sep 08, 2016
Real Time System simulation checks Completed by 08:15 hr IST. Countdown is progressing

Quote
Sep 08, 2016
N2O4 filling into four L40 Strap-On Stages completed by 03:00 hr IST

Offline vineethgk

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I used to hope that GSLV would go on to become as successful a workhorse as PSLV - but now I just hope that ISRO moves past it and keeps on iteratively improving LVM3 to better and better platforms, like an HLV


I like to see GSLV more as a test bed where ISRO really learnt the trade of rocket design. All the difficulties they encountered in the realization of the cryogenic upper stage (and a staged combustion cycle one at that ! ) and the liquid strapons would have given them a rock-solid base and confidence in growing towards LVM3 and ULV.

Offline isro-watch

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Very true, I think, GSLV-MKII used as a test-bed, most probably will be discontinued and replaced with LVM3 and versions of ULV/HLV
« Last Edit: 09/08/2016 04:23 am by isro-watch »

Offline tehwkd

One of the webcasts:
Custodian of NextLaunch & LaunchStuff |   Utilizer of Google

Offline tehwkd

another:
Custodian of NextLaunch & LaunchStuff |   Utilizer of Google

Offline Steven Pietrobon

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Livestream is starting soon. The time shown in the frame grab is my local time.
« Last Edit: 09/08/2016 10:03 am by Steven Pietrobon »
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.


Offline seshagirib

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This one says streaming in about 20mins:

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Offline seshagirib

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Looks like launch delay by about 40mins.
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Offline tehwkd

@isro announces a 40 minute delay in launch of GSLV now lift off at 4.50 pm, Cryogenic fuel filling led to delays. Countdown has resumed.

https://twitter.com/pallavabagla/status/773827023651217410

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Offline seshagirib

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Quote
Launch of GSLV-F05 carrying INSAT-3DR, an advanced weather satellite, powered by indigenous delayed roughly 40 minutes as scientists are rechecking observations made during propellant filling

source: http://timesofindia.indiatimes.com/home/science/isro-gslv-launch/liveblog/54168997.cms
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Offline worldtimedate

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10 minute delay in launching the satellite.

Launch is rescheduled to 16:50 hr IST Countdown is progressing normally

Source :
Launch is rescheduled to 16:50 hr IST Countdown is progressing normally

--- [ --- ]

Offline tehwkd

10 minute delay in launching the satellite.

Launch is rescheduled to 16:50 hr IST Countdown is progressing normally

Source :
Launch is rescheduled to 16:50 hr IST Countdown is progressing normally

--- [ --- ]

IST is UTC+5:30 as in 1650IST = 1120 UTC, still a 40min delay.
Custodian of NextLaunch & LaunchStuff |   Utilizer of Google

Offline Galactic Penguin SST

For those on GMT, that's 11:20 UTC.
Astronomy & spaceflight geek penguin. In a relationship w/ Space Shuttle Discovery.

Offline Steven Pietrobon

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A preview video is now being shown.
« Last Edit: 09/08/2016 12:28 pm by Steven Pietrobon »
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Insat 3D and Insat 3DR.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline worldtimedate

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10 minute delay in launching the satellite.

Launch is rescheduled to 16:50 hr IST Countdown is progressing normally

Source :
Launch is rescheduled to 16:50 hr IST Countdown is progressing normally

--- [ --- ]

IST is UTC+5:30 as in 1650IST = 1120 UTC, still a 40min delay.

You are right.  The launch is rescheduled at Thursday, September 08, 2016 at 07:20:00 AM  EDT  UTC-04:00

--- [ --- ]

Offline Steven Pietrobon

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Another view of the satellite. DD is showing the wrong aspect ratio on Youtube, but I'm manually correcting this in my posts.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-30 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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On the pad.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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From the control room.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-25 minutes. Showing preparation video.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Preparation screen shots.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Launch key.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-20 minutes. Launch is authorised.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Almost a green board. Bottom left is red.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Closer view.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-15 minutes. Talking about the weather.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Showing a video on Insat 3DR.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-10 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-9 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-8 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-7 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-6 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-5 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-4 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Chris Bergin

T-3 mins.
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Offline starbase

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Another view of the satellite. DD is showing the wrong aspect ratio on Youtube, but I'm manually correcting this in my posts.

One of the webcasts:

This one has correct aspect ratio.
bit.ly/SpaceLaunchCalendar ☆ bit.ly/SpaceEventCalendar

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T-3 minutes. Finally some launch video!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T-2 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Ding dong! T-1 minute.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Chris Bergin

LAUNCH!!

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Liftoff!
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T+1 minute.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Core burnout.

T+2 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Second stage ignition.

T+3 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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Fairing separation.

T+4 minutes.
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Offline Kosmos2001

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Woh! I didn't know the GSLV had such an aggressive gravity turn!  :o

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Happy with their homemade cryo stage.
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T+5 minutes.

Third stage ignition!
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T+6 minutes. Third stage performance nominal.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T+7 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T+8 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline isro-watch

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Hopefully, they hold to this view of the graphs. Gives more info than any other graph.

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T+9 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T+10 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T+11 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T+12 minutes. Performance nominal.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Chris Bergin

Performance right down the middle.
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T+13 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline isro-watch

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In Hindi, the speaker just said the vehicle's weight is 94Kg less than the previous flight !

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T+14 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T+15 minutes.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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T+16 minutes, 15 seconds.

CUS cutoff!
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Satellite separation!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Chris Bergin

Great work! Thanks very much to Steven for the excellent coverage!

Article:
https://www.nasaspaceflight.com/2016/09/indias-gslv-insat-3dr-launch/
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Separation times.
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Speeches. First operational launch.

SDSC-SHAR Director.
« Last Edit: 09/08/2016 11:41 am by Steven Pietrobon »
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Offline Shams

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Congrats to ISRO for the successful launch. Proved the reliability

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VSSC Director.
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Perigee within 300 m, apogee 80 km, 0 for inclination, 0.1 degree for argument of perigee.

LPSC Director. Virtually no anomalies.
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Vehicle Director. Naughty boy has endeared himself to India! :-)
« Last Edit: 09/08/2016 12:09 pm by Steven Pietrobon »
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Offline isro-watch

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Mr. Giri, enough of eulogizing seniors ...:)

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Next launch in March 2015 (not sure if this is for next GSLV Mk.II).

IISU Director.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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IPRC Director.
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Offline Star One

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Next launch in March 2015 (not sure if this is for next GSLV Mk.II).

IISU Director.

March 2015?

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ISAC Director. Insat 3DR has solar arrays deployed and 3 axis acquired. Scatsat launching in 2-3 weeks. Ariane on 4 October.
« Last Edit: 09/08/2016 12:12 pm by Steven Pietrobon »
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SAC Director.
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Next launch in March 2015 (not sure if this is for next GSLV Mk.II).

IISU Director.

March 2015?
Must be March 2017 for the next GSLV launch. ISRO has stated that they plan to do two GSLV flights from next year.

Offline Mapperuo

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- Aaron

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Satellite Director.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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End of broadcast. Congratulations to ISRO and India for the successful launch!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline northenarc

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 Congrats to India, three in a row for GSLV. And thanks to Steven for excellent coverage as usual.

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Next launch in March 2015 (not sure if this is for next GSLV Mk.II).

IISU Director.

March 2015?
Must be March 2017 for the next GSLV launch. ISRO has stated that they plan to do two GSLV flights from next year.

Makes sense. Unless they've discovered time travel.

Offline vineethgk

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Thanks Steve and Chris for the (as usual) wonderful coverage! Was travelling during the launch time, and depended on NSF to follow the progress..

Cheers!

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Next launch in March 2015 (not sure if this is for next GSLV Mk.II).

IISU Director.

March 2015?

I went back and listened again to the speech. At 59:20 he says "He has already demanded we fix the date of the next launch by end of March 2017." I believe that is for the next GSLV Mk.II launch.

« Last Edit: 09/08/2016 12:27 pm by Steven Pietrobon »
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline Star One

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Next launch in March 2015 (not sure if this is for next GSLV Mk.II).

IISU Director.

March 2015?

I went back and listened again to the speech. At 59:20 he says "He has already demanded we fix the date of the next launch by end of March 2017." I believe that is for the next GSLV Mk.II launch.



Thank you.

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More videos popping up online even as we speak



Somebody put it up in slo-mo for some reason

« Last Edit: 09/08/2016 12:35 pm by sanman »

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Complete launch video


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USSTRATCOM has cataloged 2 objects
(from initial TLEs)
2016-054A/41752 in 153 x 35935 km x 20.59°
2016-054B/41753 in 146 x 35757 km x 20.59°

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http://pib.nic.in/newsite/PrintRelease.aspx?relid=149636

Quote
08-September-2016 20:04 IST
GSLV Successfully Launches India’s Weather Satellite INSAT-3DR

In its tenth flight (GSLV-F05) conducted today, India's Geosynchronous Satellite Launch Vehicle, equipped with the indigenous Cryogenic Upper Stage (CUS), successfully launched the country's weather satellite INSAT-3DR, into a Geosynchronous Transfer Orbit (GTO). The achieved orbit is very close to the intended one. The launch took place from the Second Launch Pad at the Satish Dhawan Space Centre SHAR (SDSC SHAR), Sriharikota, the spaceport of India. This was the first operational flight of GSLV equipped with CUS and the fourth to carry the indigenous CUS. Today’s GSLV flight was the third consecutive success achieved by GSLV carrying indigenous CUS and the 2211 kg INSAT-3DR is the heaviest satellite to be launched from the Indian soil.

In its oval shaped GTO, the INSAT-3DR satellite is now orbiting the Earth with a perigee (nearest point to Earth) of 169.76 km and an apogee (farthest point to Earth) of 36,080.5 km with an orbital inclination of 20.62 deg with respect to the equator.

After a 29 hour 40 minutes countdown, the 415 tonne, 49 m tall GSLV-F05 carrying INSAT-3DR, lifted off at the rescheduled time of 16:50 Hrs IST. The 40 minute delay in the launch was due to an anomaly observed in the functioning of a pressure release valve in the liquid Oxygen filling ground segment which was resolved later.

At 4.8 seconds before the countdown reached zero, the four liquid propellant strap-on stages of GSLV-F05, each carrying 42 tonne of liquid propellants, were ignited. At count zero and after confirming the normal performance of all the four strap-on motors, the 139 tonne solid propellant first stage core motor was ignited and GSLV lifted off. The major phases of the flight included the core motor burn-out, strap on burn-out, ignition of the second stage, separation of the core motor together with strap-ons, payload fairing separation, second stage separation, CUS ignition and its timely shut down after satisfactory performance. About seventeen minutes after lift-off, INSAT-3DR was successfully placed in GTO.

Soon after its injection into GTO, the solar array of INSAT-3DR was automatically deployed and the Master Control Facility (MCF) at Hassan in Karnataka took control of the satellite.

Like its predecessor INSAT-3D which is providing service from orbit since 2013, INSAT-3DR is an advanced meteorological (weather observation) satellite built by India to provide a variety inputs essential for accurate weather forecasting. For this, it is equipped with three payloads (instruments), namely, a Multispectral Imager, Sounder and weather Data Relay Transponder. INSAT-3DR also carries a satellite aided Search and Rescue Transponder that picks up and relays alert signals originating from distress beacons of maritime, aviation and land based users.

In the coming days, INSAT-3DR's orbit will be raised from its present GTO to the final circular Geostationary Orbit (GSO) by firing the satellite's Liquid Apogee Motor (LAM) in stages. The satellite will be commissioned into service after the completion of orbit raising operations and the satellite’s positioning in its designated orbital slot of 74 degree East longitude in the GSO and in-orbit testing of its payloads.

Today’s flight of GSLV further highlights the success of ISRO in mastering the highly complex cryogenic rocket propulsion technology.
"Well, three cheers to Sharma, but our real baby is INSAT."

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Best ones ever posted by ISRO  ;D
« Last Edit: 09/08/2016 04:19 pm by Ohsin »
"Well, three cheers to Sharma, but our real baby is INSAT."

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Congrats to ISRO and the GSLV team. 

Thank to Steven and Chris for coverage!

 8)
"Are you sure you want to go to Red Alert, Sir? It does mean changing the bulb." - Kryten
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Quote
The operationalisation of India's heavier rocket Geosynchronous Satellite Launch Vehicle Mk II (GSLV-Mk II) opens up more launch service revenue opportunity, said a top official of Antrix Corporation Ltd.

"The GSLV rocket will operate in a different satellite launch segment. We are looking at various avenues to earn foreign exchange using this rocket," Rakesh said.

Adding to this, Indian Space Research Organisation (ISRO) Chairman A.S.Kiran Kumar said: "Antrix is also looking at launching small satellites in low orbits. Several small satellites can be accommodated in one GSLV."

Source :
ISRO puts one more rocket into global satellite launch market

--- [ --- ]

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Cryo stage video stream  8) Notice the two monitors from the right, in attached pics.
« Last Edit: 09/09/2016 03:36 am by vyoma »

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GSLV MkII F05 orbit insertion accuracy: perigee within 300m of targeted figure; apogee within 80km; inclination difference is 0°; argument of perigee difference 0.01°.

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Cryogenic stage was realized in a record time of 24 days. Launch campaign itself was just 54 working days! Next GSLV MkII launch planned in March 2017.

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Couldn't help posting the pic.. Brings out the kid in you.  ;)

Source link

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Complete launch video



At 53:43 in the launch video, the altitude and velocity plots stop updating for a few seconds.

Loss of data link ?
astronaut on space ship earth

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Any reason why ISRO skipped F03 & F05 missions when there was a continuity of Russian CUS powered operational GSLV flights ?

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Any reason why ISRO skipped F03 & F05 missions when there was a continuity of Russian CUS powered operational GSLV flights ?
My guess is that those mission numbers may have been associated to particular launches (i.e payloads) that were either delayed or did not materialize (INSAT 3D, GSAT 7 etc. ) owing to the three failed GSLV flights. ISRO seem to associate mission numbers to payloads well in advance, and do not reassign them if there are changes later, which is why the PSLV mission numbers are all jumbled up at the time of launch.

Offline vyoma

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At 53:43 in the launch video, the altitude and velocity plots stop updating for a few seconds.

Loss of data link ?

There is a continuous and overlapping telemetry coverage from launch till satellite injection, handled by various ground stations. In fact, Hindi commentator was explaining the same at that timeframe in the launch video. Brunei station covers from 700 seconds into the flight till 1000 seconds, and Biak station covers from ~960 seconds into the flight till ~1600 seconds. At 54:20 in the video, we can hear "Biak AOS" (acquisition of signal). So, I guess the ground trace plotter/blinker momentarily stopped during telemetry handover from one ground station to another, and not really due to loss of data link.
« Last Edit: 09/09/2016 07:32 am by vyoma »

Offline Stan Black

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Any reason why ISRO skipped F03 & F05 missions when there was a continuity of Russian CUS powered operational GSLV flights ?
My guess is that those mission numbers may have been associated to particular launches (i.e payloads) that were either delayed or did not materialize (INSAT 3D, GSAT 7 etc. ) owing to the three failed GSLV flights. ISRO seem to associate mission numbers to payloads well in advance, and do not reassign them if there are changes later, which is why the PSLV mission numbers are all jumbled up at the time of launch.

F03 would just be a tail number. It is not the actual serial number of the various rocket stages. You’ll find the same thing with everyone else’s rockets.

Early references point to F03 earmarked for INSAT-3D.

The last references also include mention of CUS15 and PAM upper stages. I think that it was being prepared for GLONASS?

http://forum.nasaspaceflight.com/index.php?topic=32023.msg1569474#msg1569474
http://www.bsxindia.com/SomnathProjectDirector.pdf
http://forum.nasaspaceflight.com/index.php?topic=1173.msg341952#msg341952

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ISRO also skipped GSLV D4 & went for D5 mission.
« Last Edit: 09/09/2016 08:02 am by c.hazra200 »

Offline Stan Black

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ISRO also skipped GSLV D4 & went for D5 mission.

Outcome budget 2011-2012:-
Quote
Realisation of subsystems for GSLV-D4 mission.
Launch of GSAT-D4 for in-flight validation of indigenous cyro stage (CUS-05).
Quote
GSLV-F05 (GSAT-7) and GSLV-D4 (GSAT-4R)
« Last Edit: 09/09/2016 08:27 am by Stan Black »

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Congrats ISRO on an impressive launch. Man, that rocket is chunky... a proud sight to see.

Thanks also to Steven, Chris, Ohsin, the rest of the gang for all the coverage here. Those still photos are amazing  :o is all of that falling debris ice or some type of insulation?

Offline vineethgk

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Congrats ISRO on an impressive launch. Man, that rocket is chunky... a proud sight to see.

Thanks also to Steven, Chris, Ohsin, the rest of the gang for all the coverage here. Those still photos are amazing  :o is all of that falling debris ice or some type of insulation?
Insulation I think..

Offline eeergo


[...] is all of that falling debris ice or some type of insulation?


That would be some interesting serigraphy ISRO does, considering the "ice" is painted over with the same writings as the underlying metal ;)


It's just insulation (most probably expanded polystyrene, but I don't know what they actually use) helping with the thermal conditioning of the solid and the hypergols. The third stage has its own permanent insulation, which makes it black.
-DaviD-

Offline A12

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Congrats to ISRO for a beautiful launch and impressive rocket.

Offline vyoma

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Quote
Sep 09, 2016
The first apogee raise maneuver of INSAT-3DR has been successfully carried out.

The first apogee raise maneuver of INSAT-3DR has been successfully carried out by LAM Engine firing for 2935sec from 08:39hrs IST on September 09, 2016.

Orbit Determination results from this LAM firing are:
apogee X perigee height was changed to 35882 km X 7001 km. Inclination is 9.02 deg. Orbital period is 12hr 49min.

http://www.isro.gov.in/update/09-sep-2016/first-apogee-raise-maneuver-of-insat-3dr-has-been-successfully-carried-out

Offline vyoma

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Quote
Sep 10, 2016
Second LAM firing of INSAT-3DR, at apogee for 3174sec has been successfully completed

Second LAM firing of INSAT-3DR, at apogee for 3174sec has been successfully completed on September 10, 2016 starting from 10:14hr IST.

Orbit Determination results from second LAM firing are: apogee X perigee height was changed to 35914km, 30470km Inclination is 0.419deg. Orbital period now is 21hr 45 min.

http://www.isro.gov.in/update/10-sep-2016/second-lam-firing-of-insat-3dr-apogee-3174sec-has-been-successfully-completed

Offline vyoma

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Offline seshagirib

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http://www.isro.gov.in/update/11-sep-2016/third-lam-firing-of-insat-3dr-294-sec-has-been-successfully-completed-september

Quote
Third LAM firing of INSAT-3DR for 294 sec has been successfully completed on September 11, 2016 starting from 08:31 hr IST
astronaut on space ship earth

Offline c.hazra200

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http://www.isro.gov.in/update/11-sep-2016/orbit-determination-results-third-lam-firing-are-apogee-x-perigee-height-was

Orbit Determination results from the third LAM firing are: apogee X perigee height was changed to 35908km, 35326km, Inclination is 0.121deg. Orbital period is 23hr 47m 26sec
« Last Edit: 09/11/2016 12:44 pm by c.hazra200 »

Offline c.hazra200

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In 3 orbit raising maneuvers, LAM of INSAT-3DR was fired for total of 6403 seconds where as for GSAT-6 it was fired for 6628.32 seconds i.e 225.32 seconds less than GSAT-6.
Reason ?
« Last Edit: 09/11/2016 01:12 pm by c.hazra200 »

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Offline ZachS09

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http://www.isro.gov.in/gslv-f05-insat-3dr/video-onboard-camera-of-gslv-f05

Video from onboard camera of GSLV-F05

From what I saw, there were two cameras on the second stage:

One mounted near the engine bell showing separation of the first stage and boosters.

And one mounted as a forward-facing view showing separation and ignition of the third stage.
Liftoff for St. Jude's! Go Dragon, Go Falcon, Godspeed Inspiration4!

Offline seshagirib

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http://www.isro.gov.in/gslv-f05-insat-3dr/video-onboard-camera-of-gslv-f05

Video from onboard camera of GSLV-F05

From what I saw, there were two cameras on the second stage:

One mounted near the engine bell showing separation of the first stage and boosters.

And one mounted as a forward-facing view showing separation and ignition of the third stage.

I am curious, if they, continued to capture the video until, stage breakup in the atmoshpere, or splash down, or LOS. ?
astronaut on space ship earth

Offline ZachS09

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http://www.isro.gov.in/gslv-f05-insat-3dr/video-onboard-camera-of-gslv-f05

Video from onboard camera of GSLV-F05

From what I saw, there were two cameras on the second stage:

One mounted near the engine bell showing separation of the first stage and boosters.

And one mounted as a forward-facing view showing separation and ignition of the third stage.

I am curious, if they, continued to capture the video until, stage breakup in the atmoshpere, or splash down, or LOS. ?

I dunno 'cause I don't usually follow up with the Indian Space Research Organisation.
« Last Edit: 09/15/2016 05:48 am by ZachS09 »
Liftoff for St. Jude's! Go Dragon, Go Falcon, Godspeed Inspiration4!

Offline vyoma

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Offline vineethgk

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A PDF published by ISRO with images captured by INSAT-3DR in various bands

Source

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