INSAT-4C

Launch Failure

Liftoff Time (GMT)

12:08:00

Monday July 10, 2006

Mission Details

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Launch Notes

Shortly after liftoff, a failure in the thrust controller on one of the four liquid rocket boosters resulted in an early booster shutdown. Off-axis thrust from the three remaining boosters resulted in the vehicle veering off-course. It began to disintegrate, and at T+55 seconds the Range Safety Officer terminated the flight over the Bay of Bengal. First total failure of GSLV.

INSAT-4C

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INSAT-4C was an Indian communications satellite that was lost in a launch failure in 2006. Had it reached orbit, it would have formed part of the Indian National Satellite System. Launched in 2007, it was intended to operate in geostationary orbit at a longitude of 73.97° east. The INSAT-4CR satellite, launched in September 2007, replaced it. Built by the Indian Space Research Organisation, INSAT-4C was based on the I-2K satellite bus. It had a dry mass of 950 kilograms (2,090 lb), or 2,168 kilograms (4,780 lb) when fully fuelled. It was expected to have operated for ten years. The satellite carried twelve Ku band transponders, with two solar arrays to generate power. ISRO launched INSAT-4C on the second operational flight of the Geosynchronous Satellite Launch Vehicle, which was flying in the Mk.I configuration. The launch took place from the Second Launch Pad at the Satish Dhawan Space Centre; the first time the pad was used by a GSLV. Liftoff occurred at 12:08 UTC on 10 July 2006. Early in the flight, a thrust controller in one of the four liquid rocket boosters failed, resulting in the booster cutting off shortly afterward. Approximately 55 seconds after launch the vehicle veered off-course and began to disintegrate. The range safety officer subsequently commanded the remainder of the rocket to self-destruct.

Geostationary Transfer Orbit

1 Payload

2,168 kilograms

Rocket

Retired
GSLV Mk I

Active 2001 to 2010

Indian Space Research Organisation logo

Agency

ISRO

Price

$47.00 million

Rocket

Height: 49.13m

Payload to Orbit

GTO: 1,500 kg

Fairing

Diameter: 3.4m

Height: 7.8m

Stages

3

Strap-ons

4

Launch Site

Second Launch Pad

Satish Dhawan Space Centre, India

Fastest Turnaround

31 days

Stats

GSLV Mk I & II


4th

Mission

1st

Mission of 2006

Indian Space Research Organisation


21st

Mission

1st

Mission of 2006

2006


30th

Orbital launch attempt