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LIVE: PSLV-CA C29, TeLEOS-1, December 16, 2015 12:30 UTC
by
input~2
on 18 Apr, 2015 15:01
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#1
by
input~2
on 23 Aug, 2015 20:28
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Now planned in December 2015 ( 6 satellites onboard)
(
source)
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#2
by
isro-watch
on 25 Aug, 2015 03:45
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Also mentioned in the
article is PSLV C29 launch with 6 singapore satellites by the end of year
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#3
by
Steven Pietrobon
on 25 Aug, 2015 05:03
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Also mentioned in the article is PSLV C29 launch with 6 singapore satellites by the end of year
I believe that is TeLEOS 1, VELOX C1, Kent Ridge 1 , Galassia and two other satellites.
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#4
by
Skyrocket
on 27 Aug, 2015 11:59
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Also mentioned in the article is PSLV C29 launch with 6 singapore satellites by the end of year
I believe that is TeLEOS 1, VELOX C1, Kent Ridge 1 , Galassia and two other satellites.
Correct.
Does anyone have info on the other two satellites?
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#5
by
Steven Pietrobon
on 28 Sep, 2015 09:31
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The Max Valier page is showing a countdown to 5 December 0130 UTC. My records indicated that Max Valier was going to fly on a PSLV-CA, so it might be possible this payload is going to be on this flight.
http://www.satmaxvalier.it/indexThe other payload might possibly be SkySat 3.
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#6
by
Skyrocket
on 28 Sep, 2015 09:58
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The Max Valier page is showing a countdown to 5 December 0130 UTC. My records indicated that Max Valier was going to fly on a PSLV-CA, so it might be possible this payload is going to be on this flight.
http://www.satmaxvalier.it/index
The other payload might possibly be SkySat 3.
I am not sure, as this mission goes to a low inclination orbit of 15°, which would not allow direct contact of the satellite with ground stations in northern Italy.
SkysSat 3 would likely also prefer a high inclination orbit for more coverage.
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#7
by
Steven Pietrobon
on 29 Sep, 2015 05:37
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Thanks Gunter. I had thought this launch was going into a polar orbit.
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#8
by
input~2
on 18 Oct, 2015 20:30
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#9
by
input~2
on 22 Oct, 2015 07:14
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#10
by
input~2
on 22 Oct, 2015 08:53
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Launch masses for 5 passengers on this launch :
TeLEOS-1: 400 kg
Velox C1: 135 kg
Kent Ridge 1: 80 kg
Velox II: 12 kg
Galassia: 2 kg
Total: 629 kg
(sources: NTU, NUS)
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#11
by
input~2
on 10 Nov, 2015 17:01
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#12
by
input~2
on 15 Nov, 2015 14:40
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#13
by
input~2
on 28 Nov, 2015 13:49
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#14
by
zubenelgenubi
on 03 Dec, 2015 22:37
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#15
by
m.prasad
on 04 Dec, 2015 13:51
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As per my observation, this is the 50th rocket launch from Sriharikota (considering all SLVs - SLV, ASLV, PSLV, GSLV & LVM3). Can some one validate this point?
Here are some important milestones:
01. SLV3-E1 10-Aug-1979
05. ASLV3-D1 13-Jul-1987
10. PSLV-D2 15-Oct-1994
15. PSLV-C3 22-Oct-2001
20. PSLV-C6 05-May-2005
25. PSLV-C10 21-Jan-2008
30. GSLV-D3(M2) 15-Apr-2010
35. PSLV-C18 12-Oct-2011
40. PSLV-C25 05-Nov-2013
45. GSLV-X1(M3) 18-Dec-2014
It took around ~35 years for ISRO to achieve this feat. One can observe a faster pace of launches in last few years (2nd 25 in last 7/8 years time period). Hope to see the century soon...
. I believe, ISRO will reach it within next 5-7 years time frame.
Thx
~Prasad
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#16
by
Ohsin
on 04 Dec, 2015 16:24
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04 SLV
04 ASLV
31 PSLV
09 GSLV
01 LVM3X
That is 49 flights
BUT we also had a contraption SO-300-200 that flew from Sriharikota
In the case of ASLV, Rohini rockets were used to test strap-ons. It may be recalled that ASLV was ISRO’s first launch vehicle to use strap-ons. To get some hand-on experience, ISRO rigged a Rohini strap-on rocket. The core was the RH-300 while the two strap-ons were the RH-200 rockets (only the boosters, of course). The contraption, designated as SO-300-200 was successfully flown on 16 October 1985 from Sriharikota.
Above excerpt taken from recently released book "From Fishing Hamlet to Red Planet". LVM3X and SO-300-200 both were suborbital experiments.
I think this footage(@4m30s mark) in this video is of SO-300-200.
Can't wait for Vol.2 it would have neat photographs
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#17
by
Galactic Penguin SST
on 04 Dec, 2015 17:19
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#18
by
input~2
on 04 Dec, 2015 17:26
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Back to TeLEOS-1 et al. launch:
A2333/15 - PSLV-C29 ROCKET LAUNCH FROM SHAR RANGE,SRIHARIKOTA WILL TAKEPLACE AS PER FLW DETAILS.THE LAUNCH WILL BE ON ANY ONE OF THE DAY DRG THIS PERIOD.ACTUAL DATE OF LAUNCH WILL BE INTIMATED 24 HR IN ADVANCE THROUGH A SEPARATE NOTAM. LAUNCH PAD COORD: 1343.9N 08014.2E NO FLT IS PERMITTED OVER THE DNG ZONE. A.DNG ZONE 1 A CIRCLE OF 10NM AROUND THE LAUNCHER B.DNG ZONE 2 A RECTANGULAR AREA BOUNDED BY: 1300N 08205E 1335N 08210E 1325N 08250E 1250N 08245E C.DNG ZONE 3 A RECTANGULAR AREA BOUNDED BY: 1220N 08445E 1255N 08455E 1240N 08550E 1205N 08540E D.DNG ZONE 4 A RECTANGULAR AREA BOUNDED BY: 0930N 09450E 1025N 09500E 1010N 09555E 0915N 09545E E.DNG ZONE 5 A RECTANGULAR AREA BOUNDED BY: 2100S 13400W 1900S 13400W 0800S 09400W 1000S 09400W ROUTES AFFECTED IN CHENNAI FIR ARE: N571 P761 W20 A465 P628 Q10 Q11 V003 V004 V009 AND V011 CLOSURE/ALTERNATE ROUTINGS: END PART 1 OF 2. BTN 1200-1600, 16 DEC 12:00 2015 UNTIL 15 JAN 16:00 2016. CREATED: 04 DEC 17:01 2015
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#19
by
input~2
on 04 Dec, 2015 17:38
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. I believe, ISRO will reach it within next 5-7 years time frame. 
