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GSLV-3
Part of GSLV
The Indian Geosynchronous Satellite Launch Vehicle Mark III was developed by ISRO to launch satellites into geostationary orbit and as a launcher for an Indian crew vehicle. The GSLV-3 featured an Indian cryogenic third stage and a higher payload capacity than the earlier GSLV models.
Status: Active. First Launch: 2014-12-18. Last Launch: 2018-11-14. Number: 3 .
Country:
India.
Spacecraft:
Indian Manned Spacecraft.
Launch Sites:
Sriharikota SLP.
2014 December 18 - .
04:00 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
Launch Pad: Srikarikota SLP.
LV Family:
GSLV.
Launch Vehicle:
GSLV-3.
- CARE/LVM3-X - .
Mass: 3,735 kg (8,234 lb). Nation: India.
Class: Manned.
Type: Manned spacecraft. Spacecraft: Indian Manned Spacecraft.
Apogee: 126 km (78 mi).
Launch of the first GSLV-III rocket on a suborbital test flight. The S200 solid boosters and L110 core stage, with two Vikas engines, propelled an inert second stage to 126 km and 5.3 km/s. Second stage separation and payload separation were also tested; the payload was the
Crew Module Atmospheric Reentry Experiment, a prototype command module
for an Indian manned spacecraft with a mass of 3735 kg which splashed down in the Bay of Bengal. Orbit was around -4418 x 126 km x 32.7 deg.
2017 June 5 - .
11:57 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota SLP.
LV Family:
GSLV.
Launch Vehicle:
GSLV-3.
- GSAT-19E - .
Nation: India.
USAF Sat Cat: 42747 . COSPAR: 2017-031A. Apogee: 35,805 km (22,248 mi). Perigee: 35,766 km (22,223 mi). Inclination: 0.0700 deg. Period: 1,436.05 min. See GSat 19. ..
2018 November 14 - .
11:37 GMT - .
Launch Site:
Sriharikota.
Launch Complex:
Sriharikota Dhawan SLP.
LV Family:
GSLV.
Launch Vehicle:
GSLV-3.
- GSAT-29 - .
Nation: India.
Type: Comms. USAF Sat Cat: 43698 . COSPAR: 2018-089A. Apogee: 35,797 km (22,243 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.08 min. See GSat 29. ..
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