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."
Complete launch video
Any reason why ISRO skipped F03 & F05 missions when there was a continuity of Russian CUS powered operational GSLV flights ?
At 53:43 in the launch video, the altitude and velocity plots stop updating for a few seconds.Loss of data link ?
Quote from: c.hazra200 on 09/09/2016 06:18 amAny 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.
ISRO also skipped GSLV D4 & went for D5 mission.
Realisation of subsystems for GSLV-D4 mission.Launch of GSAT-D4 for in-flight validation of indigenous cyro stage (CUS-05).
GSLV-F05 (GSAT-7) and GSLV-D4 (GSAT-4R)
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 is all of that falling debris ice or some type of insulation?
[...] is all of that falling debris ice or some type of insulation?
Sep 09, 2016The 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.
Sep 10, 2016Second LAM firing of INSAT-3DR, at apogee for 3174sec has been successfully completedSecond 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.