Author Topic: Indian sub-orbital launches  (Read 9424 times)

Offline input~2

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Indian sub-orbital launches
« on: 07/22/2016 10:02 AM »
A1571/16 -  ADVANCED TECHNOLOGY VEHICLE (ATV-D02)SOUNDING ROCKET LAUNCH FM SHAR RANGE,SRIHARIKOTA WILL TAKE PLACE AS PER FLW DETAILS. LAUNCH PAD COORD : 13 41 44 N 080 14 05 E. NO FLT IS PERMITTED OVER THE DNG ZONE. I)DANGER ZONE- 1 IS A CIRCLE OF 10NM AROUND THE LAUNCHER II)DANGER ZONE-2 IS A SECTOR BTN RADII OF 50NM AND 250NM FM THE LAUNCH PAD AND BTN AZIMUTH ANGLES 080 DEG AND 120 DEG FM TRUE NORTH ROUTES AFFECTED IN CHENNAI FIR ARE: W20,A465,N571,P761,P574,B466,L518,Q10,Q11,V3,V4,V6,V8,V9,V11,Q23 AND Q24 CLOSURE/ALTERNATE ROUTINGS: A) W20 NOT AVBL BTN MMV VOR AND BODEL ALTN ROUTE: MMV VOR-TR319/139DEG-53NM-TTP VOR-TR357/177DEG-81NM-BODEL -W20 (BIDIRECTIONAL) B) A465 NOT AVBL BTN MMV VOR AND DOCKET ALTN ROUTE:MMV VOR-TR319/139DEG-DIST 53NM-TTP VOR-VT034/214 DEG -DIST 53NM-POINT 'A'(142225N 0800303E)-TR055/235DEG-126NM-DOCKET-A465 (BIDIRECTIONAL) END PART 1 OF 2. BTN 0130-0530, 28 JUL 01:30 2016 UNTIL 11 AUG 05:30 2016. CREATED: 22 JUL 08:15 2016

Offline input~2

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Re: Indian sub-orbital launches
« Reply #1 on: 07/22/2016 07:41 PM »
Apparently the above NOTAM corresponds to a test flight for a scramjet engine
http://www.thehindu.com/todays-paper/tp-national/isro-soon-to-testfly-scramjet-engine-model/article8860925.ece

Offline Ohsin

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Re: Indian sub-orbital launches
« Reply #2 on: 07/25/2016 03:56 PM »
NOTAM is cancelled.
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Offline input~2

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Offline Ohsin

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Re: Indian sub-orbital launches
« Reply #4 on: 08/23/2016 03:49 PM »
Ready for a second attempt with slightly adjusted azimuth to adjust for under water search ops going nearby.

Quote
A1744/16 NOTAMN
Q) VOMF/QWMLW/IV/NBO/W/000/999/
A) VOMF B) 1608280030 C) 1608280430
D) BTN 0030-0430
E) ADVANCED TECHNOLOGY VEHICLE(ATV-D02) SOUNDING
ROCKET LAUNCH FM SHAR RANGE, SRIHARIKOTA WILL
TAKE PLACE AS PER FLW DETAILS:
LAUNCHPAD COORD: 134144N 0801405 E

NO FLT IS PERMITTED OVER THE DNG ZONE.
I)  DNG ZONE- 1 IS A CIRCLE OF 10NM AROUND THE LAUNCHER
II) DNG ZONE- 2 IS A SECTOR BTN RADII OF 50NM AND 220NM
    FM THE LAUNCH PAD AND BTN AZM ANGLE 070 DEG AND 100
    DEG FM TRUE NORTH
ROUTES AFFECTED IN CHENNAI FIR ARE:
W20, A465,N571,P761,L518, Q10,Q11,V4,V9,V11,Q23 AND Q24
CLOUSURE/ ALTERNATE ROUTINGS:
A) W20 NOT AVBL BTN MMV VOR AND BODEL
   ALTN RTE: MMV VOR-TR319/139DEG-53NM-TTP VOR-
   TR357/177DEG-81NM-BODEL-W20(BIDIRECTIONAL)
B) A465 NOT AVBL BTN MMV VOR AND DOKET
   ALTN RTE: MMV VOR-TR319/139 DEG-DIST 53NM-TTP VOR-
   TR034/214 DEG-DIST 53NM- POINT 'A' (142225N 0800303E)-
   TR055/235 DEG-126NM-DOKET-A465(BIDIRECTIONAL)
C) N571 NOT AVBL BTN DORAM AND BIKEN
   ALTN RTE:DORAM-DCT-MMV VOR-DCT-BIKEN-(BIDIRECTIONAL)
D) P761 NOT AVBL BTN MMV VOR AND SADAP
   ALTN RTE: MMV VOR-DCT-AVGIR-DCT-SADAP-(BIDIRECTIONAL)
E) ATS RTE Q23 BTN ISPUL AND MMV VOR NOT AVBL
   ALTN RTE: ISPUL-DCT TTP VOR-DCT-MMV VOR
F) ATS RTE Q24 BTN MMV VOR AND BODEL NOT AVBL
   ALTN RTE: MMV VOR-TTP VOR-DCT-BODEL

   ATS ROUTES L518,Q10,Q11,V4,V9,V11,NOT AVBL
F) GND G) UNL
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Offline input~2

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Re: Indian sub-orbital launches
« Reply #5 on: 08/23/2016 03:59 PM »
So new trial on August 28 from around 00:35 UTC (6:05 am IST)

Quote
BTN 0030-0430, 28 AUG 00:30 2016 UNTIL 28 AUG 04:30 2016.

Offline input~2

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Re: Indian sub-orbital launches
« Reply #6 on: 08/27/2016 08:24 AM »

Online russianhalo117

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Re: Indian sub-orbital launches
« Reply #7 on: 08/27/2016 03:47 PM »
ATV-D02 launch time announced as 6 a.m. IST (00:30 UTC) on August 28
http://www.newindianexpress.com/nation/ISRO-gears-up-to-test-scramjet-engine-on-Sunday/2016/08/27/article3599627.ece
that is start of the 4 hour launch window .

Offline Ohsin

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Re: Indian sub-orbital launches
« Reply #8 on: 08/28/2016 01:20 AM »
Quote
Kudos to @isro a futuristic Scramjet rocket tested at 6 am. ISRO Chairman Kiran Kumar tells @ndtv was a 'grand success' enjoy @PMOIndia

https://twitter.com/pallavabagla/status/769705214970441729

Edit: Blurry images it seems it was very cloudy. From following tweets

https://twitter.com/ANI_news/status/769715042669432832

https://twitter.com/mail2mugi/status/769700660245770240
« Last Edit: 08/28/2016 02:15 AM by Ohsin »
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Online Steven Pietrobon

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Re: Indian sub-orbital launches
« Reply #9 on: 08/28/2016 04:07 AM »
Here's a launch video, but I'm not sure if they are using archived footage.

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

Offline Ohsin

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Re: Indian sub-orbital launches
« Reply #10 on: 08/28/2016 05:16 AM »
That is possibly archived footage of ATV D01.

Quote
Aug 28, 2016
Successful Flight Testing of ISRO's Scramjet Engine Technology Demonstrator

The first experimental mission of ISRO’s Scramjet Engine towards the realisation of an Air Breathing Propulsion System was successfully conducted today (August 28, 2016) from Satish Dhawan Space Centre SHAR, Sriharikota.

After a smooth countdown of 12 hours, the solid rocket booster carrying the Scramjet Engines, lifted off at 0600 hrs (6:00 am) IST.  The important flight events, namely, burn out of booster rocket stage, ignition of second stage solid rocket, functioning of Scramjet engines for 5 seconds followed by burn out of the second stage took place exactly as planned.

After a flight of about 300 seconds, the vehicle touched down in the Bay of Bengal, approximately 320 km from Sriharikota. The vehicle was successfully tracked during its flight from the ground stations at Sriharikota.

With this flight, critical technologies such as ignition of air breathing engines at supersonic speed, holding the flame at supersonic speed, air intake mechanism and fuel injection systems have been successfully demonstrated.

The Scramjet engine designed by ISRO uses Hydrogen as fuel and the Oxygen from the atmospheric air as the oxidiser. Today’s test was the maiden short duration experimental test of ISRO’s Scramjet engine with a hypersonic flight at Mach 6. ISRO’s Advanced Technology Vehicle (ATV), which is an advanced sounding rocket, was the solid rocket booster used for today’s test of Scramjet engines at supersonic conditions.  ATV carrying Scramjet engines weighed 3277 kg at lift-off.

ATV is a two stage spin stabilised launcher with identical solid motors (based on Rohini RH560 sounding rocket) as the first as well as the second stage (booster and sustainer). The twin Scramjet engines were mounted on the back of the second stage. Once the second stage reached the desired conditions for engine “Start-up”, necessary actions were initiated to ignite the Scramjet engines and they functioned for about 5 seconds. Today’s ATV flight operations were based on a pre-programmed sequence.

Some of the technological challenges handled by ISRO during the development of Scramjet engine include the design and development of Hypersonic engine air intake, the supersonic combustor, development of materials withstanding very high temperatures, computational tools to simulate hypersonic flow, ensuring performance and operability of the engine across a wide range of flight speeds, proper thermal management and ground testing of the engines.

India is the fourth country to demonstrate the flight testing of Scramjet Engine. The successful technology demonstration of air-breathing Scramjet engines in flight by ISRO today is a modest yet important milestone in its endeavour to design and develop advanced air breathing engines including engines for ISRO’s future space transportation system.
http://www.isro.gov.in/update/28-aug-2016/successful-flight-testing-of-isros-scramjet-engine-technology-demonstrator
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Offline Ohsin

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Re: Indian sub-orbital launches
« Reply #12 on: 12/19/2016 11:03 AM »
Quote
The Defence Research and Development Organisation (DRDO) is gearing up for the final developmental trial of India's most potent long range nuclear capable ballistic missile, Agni-V, from a defence base off Odisha coast in the last week of December.

Defence sources said the trial is significant as it will be the first test of a long range missile after the country joined the Missile Technology Control Regime (MTCR)

http://www.newindianexpress.com/nation/2016/dec/14/final-developmental-test-of-5000-km-range-agni-v-soon-1549110.html

Quote
A2696/16 NOTAMN
Q) VOMF/QWMLW/IV/BO/W/000/999/
A) VOMF/VECF PART 1 OF 3 B) 1612260300 C) 1612270700
D) 0300-0700
E) EXPERIMENTAL FLIGHT VEHICLE LAUNCH WILL TAKE PLACE WITH THE FLW
DETAILS:   
THE COORDS OF THE DANGER ZONES A AND B ARE AS FOLLOWS:
DANGER ZONE ?A?
        POINT A1: 204821N   0870234
        POINT A2: 190323N   0862618
        POINT A3: 062159S   0870517
        POINT A4 : 061622S  0892153
        POINT A5:  055934S  0913732
        POINT A6: 191117N   0880220
        POINT A7?  204845N  0870724E
        POINT A1:  204821N   0870234
END PART 1 OF 3

A2696/16 NOTAMN
Q) VOMF/QWMLW/IV/BO/W/000/999/
A) VOMF/VECF PART 2 OF 3 B) 1612260300 C) 1612270700
D) 0300-0700
E) DANGER ZONE ?B?
        POINT B1: 152410S   0873808E
        POINT B2: 251925S   0882606
        POINT B3: 251049S   0910234
        POINT B4 :245347S   0933757
        POINT B5: 145939S   0923553
        POINT B1: 152410S   0873808
NO OVERFLYING ACTIVITY IS PERMISSIBLE WI THE ABOVE
MENTIONED AREAS DURING THE HOURS OF LAUNCH THE FOLLOWING ATS ROUTES
ARE  REROUTED / NOT AVBL:
END PART 2 OF 3

Plotted https://drive.google.com/open?id=1g9JScPuuzQp35P3qqtWT7XODxRM

HSTDV(scramjet) was also planned this December from news reports few months old.
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Offline input~2

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Re: Indian sub-orbital launches
« Reply #13 on: 01/30/2017 04:22 PM »
A0158/17 -  EXPERIMENTAL FLT VEHICLE LAUNCH WILL TAKE PLACE WITH THE FLW DETAILS: THE COORD OF THE DNG ZONES POLYGON ARE AS FLW: POLYGON A POINT A1: 174131.20N   0833926.64E POINT A2: 150203.12N   0825931.56E POINT A3: 032626.88N0862600.60E POINT A4 : 045418.00N  0903903.60E POINT A5: 160509.96N  0860038.16E POINT A6: 174304.80N  0834354.48E POINT A1: 174131.20N 0833926.64E POLYGON B POINT B1:064216.20S0884354.84E POINT B2: 104126.16S  0893307.20E POINT B3: 080825.08S  0965339.12E POINT B4 :043025.56S  0950345.00E POINT B1: 064216.20S  0884354.84E NO OVERFLYING ACT PERMISSIBLE WI THE ABOVE MENTIONED AREA. DRG THE HOURS OF LAUNCH THE FLW ATS ROUTES ARE REROUTED / NOT AVBL. 1. A465 NOT AVBL BTN VVZ VOR  AND LARIK ALTN RTE: VVZ VOR-DCT-POINT 'P' (1756N 08322E)-DCT LARIK (BIDIRECTIONAL) 2. N877 NOT AVBL BTN SADAP AND RIBRO ALTN RTE: SADAP-DCT- BIDEX--L510-DCT -NIKIR- DCT- RIBRO (BIDIRECTIONAL). ONLY FL300 AND FL340  AVBL FOR WB FLIGHTS ON ALTN RTE OF N877.OTHER WB LEVELS AVBL ON ACCEPTANCE BASIS.   NO LVL RESTRICTIONS FOR EB FLIGHTS. 3. W47/A465 NOT AVBL BTN VVZ VOR AND LARIK(ACFT OVERFLYING VVZ VOR) VVZ VOR-DCT-POINT 'P'(1756N 08322E)-DCT LARIK (BIDIRECTIONAL. 0630-1030, 30 JAN 06:30 2017 UNTIL 31 JAN 10:30 2017. CREATED: 27 JAN 12:39 2017

BAY OF BENGAL AND NORTH INDIAN OCEAN – CHARTS 31 INT 71 (.) EXPERIMENTAL
FLIGHT TRIAL SCHEDULED FROM ITR DAILY FROM 30 JAN TO 01 FEB17 FROM 0630-1030 UTC
IN DANGER ZONE BOUNDED BY 17-41.52N 083-39.44E, 15-02.05N 082-59.53E, 03-26.45N
086-26.01E, 04-54.30N 090-39.06E, 16-05.17N 086-00.64E, 17-43.08N 083-43.91E AND 06-42.27S
088-43.91E, 10-41.44S 089-33.12E, 08-08.42S 096-53.65E, 04-30.43S 095-03.75E

INDIAN OCEAN.
BAY OF BENGAL.
INDIA.
DNC 03.
1. HAZARDOUS OPERATIONS 0630Z TO 1030Z DAILY
30 JAN THRU 01 FEB IN AREAS BOUND BY:
A. 17-41.52N 083-39.44E, 15-02.05N 082-59.53E,
03-26.45N 086-26.01E, 04-54.30N 090-39.06E,
16-05.17N 086-00.64E, 17-43.08N 083-43.91E.
B. 06-42.27S 088-43.91E, 10-41.44S 089-33.12E,
08-08.42S 096-53.65E, 04-30.43S 095-03.75E.
2. CANCEL HYDROPAC 276/17.
3. CANCEL THIS MSG 011130Z FEB 17.//

Authority: NAVAREA VIII 70/17 271025Z JAN 17.

Date: 271032Z JAN 17
Cancel: 01113000 Feb 17

« Last Edit: 01/30/2017 04:48 PM by input~2 »

Offline eeergo

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Offline input~2

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Re: Indian sub-orbital launches
« Reply #15 on: 01/31/2018 01:59 PM »
A0205/18 -  LAUNCHING OF EXPERIMENTAL FLT VEHICLE WILL TAKE PLACE. DNG ZONES COORD: POINT A - 212212.36N 0865542.96E POINT B - 210843.44N 0865338.40E POINT C - 192419.44N 0865750.40E POINT D - 145528.92N 0874924.60E POINT E - 152002.40N 0892700.72E POINT F - 192719.08N 0891422.20E POINT G - 212146.80N 0871051.24E POINT H - 212241.16N 0865620.76E POINT A - 212212.36N 0865542.96E NO OVER FLYING ACT IS PERMISSBLE WI THE ABOVE MENTIONED AREAS.DRG THE HR OF LAUNCH ,THE FLW ATS RTE/SEGMENTS ARE REROUTED/NOT AVBL IN CHENNAI FIR. 1. L510 NOT AVBL BTN DOGEM AND BASOP. ALTN RTE : DOGEM -DCT SADAP-DCT-BASOP.(ALTERNATE ROUTING EAST BOUND ONLY) 2. P628 NOT AVBL BTN PPB VOR AND ASOPO. ALTN RTE: PPB VOR-W112-DOPID-CEA VOR -A791-ASOPO(BIDIRECTIONAL) ONLY F280 AVBL FOR WB FLTS.OTHER FLT LEVELS ARE AVBL ON ACCEPTANCE BASIS 3. A465 NOT AVBL BTN VVZ VOR AND CEA VOR. ALTN RTE: VVZ VOR -DCT MEPOL-W41-BBS VOR-W50-JH-DCT-AGROM-G450- CEA VOR(BIDIRECTIONAL) 4. Q10 NOT AVBL 5. Q11 NOT AVBL 6. W111 NOT AVBL BTN VATLA AND DOPID. GND - UNL, 0230-0630 06 AND 08, 06 FEB 02:30 2018 UNTIL 08 FEB 06:30 2018. CREATED: 30 JAN 09:01 2018
« Last Edit: 02/08/2018 07:24 PM by input~2 »

Offline Satori

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Re: Indian sub-orbital launches
« Reply #16 on: 02/06/2018 03:26 PM »
India test fire Nuclear-capable Agni-I missile.

Agni-I missile with nuclear weapon carrying capability flight-tested successfully.

edit by input~2: was conducted on Tuesday Feb 6, am LT (supposedly linked to NOTAM above)
« Last Edit: 02/22/2018 03:34 PM by input~2 »

Offline input~2

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Re: Indian sub-orbital launches
« Reply #17 on: 02/08/2018 07:21 PM »
A0259/18 -  EXPERIMENTAL FLT VEHICLE LAUNCH WILL TAKE PLACE WITH THE FLW DETAILS: THE COORD OF THE DNG ZONE POLYGON ARE AS FLW: POLYGON ?A POINT A1: 174431.92N   0832952.44 POINT A2: 150155.56N   0825500.84 POINT A3: 032656.76N   0862337.68 POINT A4 : 045533.60N  0903625.20 POINT A5: 160535.16N  0855555.56 POINT A6: 174812.24N  0834017.40E POINT A1:  174431.92N   0832952.44 POLYGON ?B? POINT B1: 064216.20S   0884354.84E POINT B2: 104126.16S  0893307.20 POINT B3: 080825.08S  0965339.12 POINT B4 :043025.56S  0950345.00 POINT B1: 064216.20S  0884354.84E NO OVERFLYING ACT IS PERMISSIBLE WI THE ABOVE MENTIONED AREA DRG THE HOURS OF LAUNCH THE FLW ATS ROUTES ARE REROUTED / NOT AVBL: 1.   A465 NOT AVBL BTN XOPOX   AND LARIK ALTN RTE: XOPOX-DCT-POINT P 1810N 08316E-DCT LARIK (BIDIRECTIONAL) 2.   N877 NOT AVBL BTN SADAP AND RIBRO ALTN RTE: SADAP-DCT- BIDEX--L510-DOGEM-NIKIR- DCT- RIBRO (BIDIRECTIONAL. DLY 0630-1030, 15 FEB 06:30 2018 UNTIL 17 FEB 10:30 2018. CREATED: 06 FEB 05:05 2018


F0261/18 -  INDIAN EXPERIMENTAL FLIGHT VEHICLE LAUNCH IS SKED TO TAKE PLACE WITHIN THE FOLLOWING DANGER ZONE WHICH ENCROACHES THE MELBOURNE FLIGHT INFORMATION REGION (FIR) THE ROCKET HAS BEEN SCHEDULED FROM 15 FEBRUARY TO 17 FEBRUARY 2018. DANGER TIMES ARE FROM 0630UTC TO 1030UTC DAILY THE DANGER ZONE IS BOUNDED BY THE FOLLOWING COORDINATES: 064216.20S  0884354.84E 104126.16S  0893307.20E 080825.08S  0965339.12E 043025.56S  0950345.00E 064216.20S  0884354.84E. SFC - UNL, DAILY 0630/1030, 15 FEB 06:30 2018 UNTIL 17 FEB 10:30 2018. CREATED: 29 JAN 16:23 2018
« Last Edit: 02/08/2018 07:35 PM by input~2 »

Online jcm

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Re: Indian sub-orbital launches
« Reply #18 on: 02/22/2018 04:27 AM »
A0259/18 -  EXPERIMENTAL FLT VEHICLE LAUNCH WILL TAKE PLACE WITH THE FLW DETAILS: THE COORD OF THE DNG ZONE POLYGON ARE AS FLW: POLYGON ?A POINT A1: 174431.92N   0832952.44 POINT A2: 150155.56N   0825500.84 POINT A3: 032656.76N   0862337.68 POINT A4 : 045533.60N  0903625.20 POINT A5: 160535.16N  0855555.56 POINT A6: 174812.24N  0834017.40E POINT A1:  174431.92N   0832952.44 POLYGON ?B? POINT B1: 064216.20S   0884354.84E POINT B2: 104126.16S  0893307.20 POINT B3: 080825.08S  0965339.12 POINT B4 :043025.56S  0950345.00 POINT B1: 064216.20S  0884354.84E NO OVERFLYING ACT IS PERMISSIBLE WI THE ABOVE MENTIONED AREA DRG THE HOURS OF LAUNCH THE FLW ATS ROUTES ARE REROUTED / NOT AVBL: 1.   A465 NOT AVBL BTN XOPOX   AND LARIK ALTN RTE: XOPOX-DCT-POINT P 1810N 08316E-DCT LARIK (BIDIRECTIONAL) 2.   N877 NOT AVBL BTN SADAP AND RIBRO ALTN RTE: SADAP-DCT- BIDEX--L510-DOGEM-NIKIR- DCT- RIBRO (BIDIRECTIONAL. DLY 0630-1030, 15 FEB 06:30 2018 UNTIL 17 FEB 10:30 2018. CREATED: 06 FEB 05:05 2018


F0261/18 -  INDIAN EXPERIMENTAL FLIGHT VEHICLE LAUNCH IS SKED TO TAKE PLACE WITHIN THE FOLLOWING DANGER ZONE WHICH ENCROACHES THE MELBOURNE FLIGHT INFORMATION REGION (FIR) THE ROCKET HAS BEEN SCHEDULED FROM 15 FEBRUARY TO 17 FEBRUARY 2018. DANGER TIMES ARE FROM 0630UTC TO 1030UTC DAILY THE DANGER ZONE IS BOUNDED BY THE FOLLOWING COORDINATES: 064216.20S  0884354.84E 104126.16S  0893307.20E 080825.08S  0965339.12E 043025.56S  0950345.00E 064216.20S  0884354.84E. SFC - UNL, DAILY 0630/1030, 15 FEB 06:30 2018 UNTIL 17 FEB 10:30 2018. CREATED: 29 JAN 16:23 2018

This could be the Agni 2 launch which happened Feb 20 https://economictimes.indiatimes.com/news/defence/india-test-fires-agni-ii-missile-off-odisha-coast/articleshow/62993975.cms
-----------------------------

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Offline input~2

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Re: Indian sub-orbital launches
« Reply #19 on: 02/22/2018 03:50 PM »
A0259/18 -  EXPERIMENTAL FLT VEHICLE LAUNCH WILL TAKE PLACE WITH THE FLW DETAILS: THE COORD OF THE DNG ZONE POLYGON ARE AS FLW: POLYGON ?A POINT A1: 174431.92N   0832952.44 POINT A2: 150155.56N   0825500.84 POINT A3: 032656.76N   0862337.68 POINT A4 : 045533.60N  0903625.20 POINT A5: 160535.16N  0855555.56 POINT A6: 174812.24N  0834017.40E POINT A1:  174431.92N   0832952.44 POLYGON ?B? POINT B1: 064216.20S   0884354.84E POINT B2: 104126.16S  0893307.20 POINT B3: 080825.08S  0965339.12 POINT B4 :043025.56S  0950345.00 POINT B1: 064216.20S  0884354.84E NO OVERFLYING ACT IS PERMISSIBLE WI THE ABOVE MENTIONED AREA DRG THE HOURS OF LAUNCH THE FLW ATS ROUTES ARE REROUTED / NOT AVBL: 1.   A465 NOT AVBL BTN XOPOX   AND LARIK ALTN RTE: XOPOX-DCT-POINT P 1810N 08316E-DCT LARIK (BIDIRECTIONAL) 2.   N877 NOT AVBL BTN SADAP AND RIBRO ALTN RTE: SADAP-DCT- BIDEX--L510-DOGEM-NIKIR- DCT- RIBRO (BIDIRECTIONAL. DLY 0630-1030, 15 FEB 06:30 2018 UNTIL 17 FEB 10:30 2018. CREATED: 06 FEB 05:05 2018



F0261/18 -  INDIAN EXPERIMENTAL FLIGHT VEHICLE LAUNCH IS SKED TO TAKE PLACE WITHIN THE FOLLOWING DANGER ZONE WHICH ENCROACHES THE MELBOURNE FLIGHT INFORMATION REGION (FIR) THE ROCKET HAS BEEN SCHEDULED FROM 15 FEBRUARY TO 17 FEBRUARY 2018. DANGER TIMES ARE FROM 0630UTC TO 1030UTC DAILY THE DANGER ZONE IS BOUNDED BY THE FOLLOWING COORDINATES: 064216.20S  0884354.84E 104126.16S  0893307.20E 080825.08S  0965339.12E 043025.56S  0950345.00E 064216.20S  0884354.84E. SFC - UNL, DAILY 0630/1030, 15 FEB 06:30 2018 UNTIL 17 FEB 10:30 2018. CREATED: 29 JAN 16:23 2018

This could be the Agni 2 launch which happened Feb 20 https://economictimes.indiatimes.com/news/defence/india-test-fires-agni-ii-missile-off-odisha-coast/articleshow/62993975.cms

More likely this one below for Feb 20, 02:30-06:30 UTC as launch was reported in the article with a T0:  Feb 20 at 03:08 UTC

A0304/18 NOTAMN 
Q) VOXX/QWMLW/IV/BO /W /000/999/
A) VOMF/VECF PART 1 OF 2 B) 1802200230 C) 1802221600   
D) 20 0230-0630
22 0230-0430 AND 1400-1600
E) EXPERIMENTAL FLT VEHICLE LAUNCH WILL TAKE PLACE
WITH THE FLW DETAILS:
COORDS OF THE DNG ZONES ARE AS FLW:-
POINT A : 212218.48N 0865545.12E
POINT B : 210917.64N 0865127.36E
POINT C : 181220.52N 0860708.40E
POINT D : 071255.44N 0862303.84E
POINT E : 073122.44N 0900708.76E
POINT F : 184731.20N 0891142.72E
POINT G : 211939.72N 0871037.92E
POINT H : 212241.16N 0865627.24E
POINT A : 212218.48N 0865545.12E

NO OVERFLYING ACT IS PERMISSIBLE WI THE ABOVE MENTIONED
AREAS DRG THE HR OF LAUNCH.
THE FLW ATS RTE ARE REROUTED/NOT AVBL
1. A465 NOT AVBL BTN VVZ VOR AND CEA VOR
   ALTN RTE : VVZ VOR-DCT-MEPOL-W41-BBS VOR-W50-JH-DCT-
   AGROM-G450-CEA VOR (BIDIRECTIONAL)
END PART 1 OF 2

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