PSLV
ActiveIndian Space Research Organization (ISRO)
April 23, 2007
Description
The PSLV-CA, CA meaning "Core Alone", model premiered on 23 April 2007. The CA model does not include the six strap-on boosters used by the PSLV standard variant. The fourth stage of the CA variant has 400 kg less propellant when compared to its standard version. It currently has capability to launch 1,100 kg to a 622 km Sun synchronous orbit.
Specifications
-
Stages
4 -
Length
44.0 m -
Diameter
2.8 m -
Fairing Diameter
3.2 m -
Launch Mass
230.0 T -
Thrust
4847.0 kN
Family
-
Name
PSLV -
Family
― -
Variant
CA -
Alias
― -
Full Name
PSLV-CA
Payload Capacity
-
Launch Cost
$16000000 -
Low Earth Orbit
3800.0 kg -
Geostationary Transfer
Orbit
1200.0 kg -
Direct Geostationary
― -
Sun-Synchronous Capacity
1092.0 kg
Indian Space Research Organization
Government
Chairman: V. Narayanan
ISRO 1969The Indian Space Research Organisation (ISRO) is the space agency of the Government of India headquartered in the city of Bangalore. Its vision is to "harness space technology for national development while pursuing space science research and planetary exploration."
PSLV-CA | SPADEX (Space Docking Experiment)
Indian Space Research Organization | IndiaSatish Dhawan Space Centre, India
Dec. 30, 2024, 4:30 p.m.
Status: Launch Successful
Mission:
SPADEX (Space Docking Experiment) is an Indian Space Research Organisation (ISRO) technology mission to demonstrate autonomous docking between 2 spacecraft in orbit. The mission will involve two spacecraft (Chaser and Target) rendezvous and docking together, plus testing attitude control of the combined spacecraft under docked conditions. The Chaser and Target spacecraft will then be separated for operating other payload. The mission is critical to develop rendezvous and docking abilities for ISRO’s future human spaceflight and lunar sample return missions.
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