Explore

VIKRAM

Series

Vikram, named after Dr. Vikram Sarabhai, the father of Indian Space Program, is a series of launch vehicles especially crafted for the small satellite market. Built on common architecture and covering a wide range of payloads, they offer the most affordable and on demand ride to space.   

Launch Vehicles

Vikram I
Vikram II
Vikram III

 

PAYLOAD

225 kg to 500 km SSPO.
315 kg to 45º inclination 500 km LEO .

ARCHITECTURE

Highly reliable solid propulsion stages with proven design heritage.
Miniaturized and Modern Avionics.
Ultra-Lowshock Pneumatic separation.

FLEXIBLE

Orbital Adjustment Module with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 24 hours from any launch site.

 

PAYLOAD

410 kg to 500 km SSPO.
520 kg to 45º inclination 500 km LEO .

ARCHITECTURE

Advanced Cryogenic Methalox engine replaces third stage of Vikram 1 .

FLEXIBLE

Upper stage cryo-engine with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 72 hours from any launch site.

 

PAYLOAD

580 kg to 500 km SSPO.
720 kg to 45º inclination 500 km LEO .

ARCHITECTURE

An Upgrade to Vikram 2 With Additional low cost Strapped on Solid Rocket Boosters

FLEXIBLE

Upper stage engine with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 72 hours from any launch site.

Explore

VIKRAM

Series

Vikram, named after Dr. Vikram Sarabhai, the father of Indian Space Program, is a series of launch vehicles especially crafted for the small satellite market. Built on common architecture and covering a wide range of payloads, they offer the most affordable and on demand ride to space.   

Launch Vehicles

Vikram I
Vikram II
Vikram III

 

PAYLOAD

225 kg to 500 km SSPO.
315 kg to 45º inclination 500 km LEO .

ARCHITECTURE

Highly reliable solid propulsion stages with proven design heritage.
Miniaturized and Modern Avionics.
Ultra-Lowshock Pneumatic separation.

FLEXIBLE

Orbital Adjustment Module with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 24 hours from any launch site.

 

PAYLOAD

410 kg to 500 km SSPO.
520 kg to 45º inclination 500 km LEO.

ARCHITECTURE

Advanced Cryogenic Methalox engine replaces third stage of Vikram 1.

FLEXIBLE

Upper stage cryo-engine with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 72 hours from any launch site.

 

PAYLOAD

580 kg to 500 km SSPO.
720 kg to 45º inclination 500 km LEO .

ARCHITECTURE

An Upgrade to Vikram 2 With Additional low cost Strapped on Solid Rocket Boosters

FLEXIBLE

Upper stage engine with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 72 hours from any launch site.

Vikram I
Vikram II
Vikram III

PAYLOAD

200 kg to 500 km SSPO.
280 kg to 45º inclination 500 km LEO .

ARCHITECTURE

Highly reliable solid propulsion stages with proven design heritage.
Miniaturized and Modern Avionics.
Ultra-Lowshock Pneumatic separation.

FLEXIBLE

Orbital Adjustment Module with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 24 hours from any launch site.

PAYLOAD

410 kg to 500 km SSPO.
520 kg to 45º inclination 500 km LEO .

ARCHITECTURE

Advanced Cryogenic Methalox engine replaces third stage of Vikram 1 .

FLEXIBLE

Upper stage cryo-engine with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 72 hours from any launch site.

PAYLOAD

580 kg to 500 km SSPO.
720 kg to 45º inclination 500 km LEO .

ARCHITECTURE

An Upgrade to Vikram 2 With Additional low cost Strapped on Solid Rocket Boosters

FLEXIBLE

Upper stage engine with re-start capability enables multi-orbit insertions.

ECONOMIC

Lowest cost in the payload segment

RESPONSIVE

Requires Minimal range infrastructure. Can be assembled and launched within 72 hours from any launch site.