![]() | |
PSLV-XL launch | |
---|---|
Launch | 14 February 2022IST | , 05:59:00
Pad | Sriharikota First |
Payload |
![]() ![]() ![]() ![]() ![]() |
Outcome | Success |
PSLV launches | |
The PSLV-C52 [1] is the 54th mission of the Indian Polar Satellite Launch Vehicle (PSLV) program. The Polar Satellite Launch Vehicle (PSLV)-C52 was launched at 05:59 ( IST) on 14 February 2022 with the RISAT-1A(EOS-04), INSPIREsat, INS-2TD as its main payload. [2]
The PSLV-C52 was launched from the First Launch Pad of the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh,India. The PSLV C52 rocket carried primary payload, RISAT-1A with 2 other satellites. These will be the INSPIREsat from the IIST and the INS-2TD technology demonstrator from ISRO. [3] [2]
The PSLV-C52 was launched at 5:59 ( IST) on 14 February 2022.
The PSLV C52 rocket has four stages; each one was self-contained, with its own
propulsion system, thereby capable of functioning independently. The first and third stages used composite solid propellants, while the second and fourth stage use earth-storable liquid propellant.
[1]
![]() | |
PSLV-XL launch | |
---|---|
Launch | 14 February 2022IST | , 05:59:00
Pad | Sriharikota First |
Payload |
![]() ![]() ![]() ![]() ![]() |
Outcome | Success |
PSLV launches | |
The PSLV-C52 [1] is the 54th mission of the Indian Polar Satellite Launch Vehicle (PSLV) program. The Polar Satellite Launch Vehicle (PSLV)-C52 was launched at 05:59 ( IST) on 14 February 2022 with the RISAT-1A(EOS-04), INSPIREsat, INS-2TD as its main payload. [2]
The PSLV-C52 was launched from the First Launch Pad of the Satish Dhawan Space Centre in Sriharikota, Andhra Pradesh,India. The PSLV C52 rocket carried primary payload, RISAT-1A with 2 other satellites. These will be the INSPIREsat from the IIST and the INS-2TD technology demonstrator from ISRO. [3] [2]
The PSLV-C52 was launched at 5:59 ( IST) on 14 February 2022.
The PSLV C52 rocket has four stages; each one was self-contained, with its own
propulsion system, thereby capable of functioning independently. The first and third stages used composite solid propellants, while the second and fourth stage use earth-storable liquid propellant.
[1]