NEXT SPACEFLIGHT

Status

Success

IRS-1C & Skipper

Launch Time
Thu Dec 28, 1995 06:45 UTC

Rocket

Molniya-M/Block 2BL
Image Credit: VKS RF
VKS RF
Status: Retired
Liftoff Thrust: 4,391 kN
Payload to LEO: 6,200 kg
Payload to GTO: 2,400 kg
Stages: 4
Strap-ons: 4
Rocket Height: 44.23 m
Fairing Diameter: 2.58 m
Fairing Height: 7.81 m

Mission Details

IRS-1C

IRS 1C and 1D (Indian Remote Sensing Satellite) were the second version of the series of indigenous state-of-art remote sensing satellites.

These satellites carried payloads with enhanced capabilities like better spatial resolution additional spectral band, improved repetitivity and augment the remote sensing capability of the first generation IRS-1A and IRS-1B. The payload consisted of three solid state push broom cameras.

Payloads: 1
Total Mass: 1,250.0 kg
Sun-Synchronous Orbit

Skipper

Skipper was an international project initiated by BMDO to measure the bow-shock UV emissions from reentering bodies at different speeds and heights.

Skipper was the third mission in BMDO's Bowshock program. The first two Bowshock missions were suborbital flights on sounding rockets.

The instruments and the bus were built in the USA by the Space Dynamics Laboratory, while the propulsion module, solar power systems were built in Russia by Moscow Aviation Institute (RIAME/MAI).

Payloads: 1
Total Mass: 230.0 kg
Sun-Synchronous Orbit

Location

Site 31/6, Baikonur Cosmodrome, Kazakhstan

Stats

1995

78th orbital launch attempt

Molniya-M

257th mission
4th mission of 1995
243rd successful mission
34th consecutive successful mission