ST 8

ST 8 [OSC] |
The ST8 (Space Technology 8) Mission, slated for launch in 2009, is a
New Millennium Carrier that will host a varied payload of four advanced technologies. Each
technology validation experiment will include diagnostic instruments. They will perform
detailed measurements to characterize and determine how well the technologies performance
in space corresponds to predictions derived from ground-based testing and modeling. The
resulting data will be provided to science mission planners to enable a broad range of
space-based science projects at significantly reduced risk and cost. The selected suite of
advanced technology experiments includes:
- Ultraflex Next Generation Solar Array System (NGU) from AEC-Able Engineering, Inc.,
Goleta, Calif. The NGU is an ultra-lightweight flexible-blanket solar array that deploys
to provide a significant advancement in performance over existing state-of-the-art for
high power arrays. The proposed experiment cost for the NGU is $6.9 million.
- SAILMAST Ultra Lightweight Boom from AEC-Able Engineering, Inc. The SAILMAST is an
ultra-light graphite mast intended for solar sail propulsion systems. The proposed
experiment cost for the SAILMAST is $4 million.
- Miniature Loop Heat Pipe Small Spacecraft Thermal Management System (MLHP) from NASA's
Goddard Space Flight Center, Greenbelt, Md. The MLHP can transport large heat loads over
long distances with small temperature differences and without external pumping powers to
provide precise temperature control and reduce the need for supplemental heaters. The
proposed experiment cost for the MLHP is $9.8 million.
- Environmentally Adaptive Fault Tolerant Computing System (EAFTC) from Honeywell
International, Inc., Clearwater, Fla. The EAFTC will provide high rate on board processing
for science data and autonomous control functions. The proposed experiment cost for the
EAFTC is $10 million.
ST8 was planned for a 2009 Pegasus-XL
launch, but has been cancelled.
| Nation: |
USA |
| Type / Application: |
Technology |
| Operator: |
NASA |
| Contractors: |
Orbital Sciences Corporation (OSC) |
| Equipment: |
NGU, SAILMAST, MLHP, EAFTC |
| Configuration: |
MicroStar-2 |
| Propulsion: |
? |
| Lifetime: |
7 months |
| Mass: |
246 kg |
| Orbit: |
450 km x 955 km SSO |
| Satellite |
Date |
LS |
|
Launcher |
Remarks: |
| ST 8 |
cancelled |
Va |
|
Pegasus-XL |
|
| Further New Millennium Missions:
|
Source: NASA press release
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs