MSX

USA


Midcourse Space Experiment

Launch data:

Designation 23851 / 96024A
Launch date 24 Apr 1996
Launch site Va, SLC-2W
Launch vehicle  Delta-7920-10 (#D235)
Operator Ballistic Missile Defense Organization (BMDO)
Mission  
Earth orbit:
Perigee/Apogee 896/906 km
Inclination 99°
Period  
Mass at launch 2600 kg

Johns Hopkins University's Applied Physics Laboratory built the MSX spacecraft for the BMDO. The Spirit III cryogenic-cooled infrared sensor system was supplied to BMDO by Utah State University/Space Dynamics Laboratory.


Mission details:

The prime objective of the MSX satellite was to test methods to detect, track and discriminate missiles during mid-course stages of their flight against terrestrial Earth limb and celestial backgrounds. MSX will also perform civilian scientific research, with atmospheric observations and astronomical studies. It will provide data on small debris in space. The satellite had a mass of 2680 kg and the instruments were:


Telemetry: 2282.5 MHz
Data: 8475.0 MHz

As part of the scientific programme the satellite tracked missiles fired from the Kauai Test Facility and Vandenberg. It also tracked Cosmos-1278, Cosmos-2227 and a Titan transtage. It has been reported that on 24 August 1996 and 12 September 1996 two small calibration satellites were released, however, it does not appear these have been catalogued.

The Midcourse Space Experiment (MSX) programme also involved various Space Shuttle flights, commencing with STS-63. After the programme was completed, in 1998, the satellite was used to locate 'missing' satellites for NORAD.


Payload

SPIRIT III: 0.34m Spatial IR Imaging Telescope, 2.5 -28 microns
UVISI: UV and Visible Imagers and Spectrographic Imagers
CIC: Contamination Instrumentation Complement (to study outgassing and contamination of optical surfaces)
SBV: Space Based Visible camera, 0.15m telescope/CCD

Spirit III is the first cryogenic infrared telescope to use solid hydrogen instead of the liquid helium that has been used by infrared astronomy satellites in the past. The hydrogen will maintain the dewar at 8.5K.


Ref: #15, #99 - update: 01.07.05