Jason 1

FR & US


Spacecraft n°:

US satellite n°:


Launch data:

Designation 26997 / 01055A
Launch date 07 Dec 2001 - 15:07:35 UT
Launch site Va, SLC2W
Launch vehicle Delta 7920-10(#D289)
MissionRemote sensing
Perigee/Apogee 1337 km
Inclination 66°
Period 112 min (9.9 days repeat)


Is to replace Topex Poseidon but will fly in formation for a while. Launch was delayed to after a problem in a solar array drive motor was detected. Was declared operational in March 2002. Control of the satellite should be transfered to JPL in April 2002.

Specifications

Prime contractor Alcatel Space
Platform Proteus
Mass at launch 500 kg
Mass in orbit  
Dry mass 472 kg
Dimension  
Solar array Twin panels, provide 1000 W
Stabilization 3-axis
DC power EOL: 1000 W
Design lifetime 5 years


Payload


Poseidon 2 (CNES): dual frequency radar altimetry to be built by Alcatel Telecom for about $29 million
Doris (CNES)
JMR (NASA)
TRSR
LRA -NASA)

Should downlink in S-band atr 613 Kbps over Poker Flats, Alaska and Wallops Island, Virginia.


Ref: #7, #15, #98a - update: 22.10.08