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XSS-10
microsatellite is an auxiliary payload which will be used to
demonstrate satellite navigation technology and inspect the Delta
2's second stage after it separates. The experimental
micro-satellite is attached to the second stage. The XSS-10 craft
will separate from the spent stage about 16 hours after launch to
perform autonomous maneuvers around the rocket body for several
hours. The entire mission will last approximately 24 hours. The
XSS-10 is the first in a series of future micro-satellites the
USAF plans to use for inspection, rendezvous and docking and
close-up maneuvering around other space objects. The Air Force
Research Laboratory (AFRL) is building and demonstrating this new
class of low-cost “micro” satellites. This satellites is being
flown under the Experimental Spacecraft System (XSS)
Microsatellite Demonstration Project.
| XSS-10
|
|
SPACECRAFT
|
| Int'l Designation |
2003 005B
|
Scheduled
|
| Owner / Sponsor |
U.S.
Air Force Research Lab (AFRL)
|
| Mission |
Technology
Demonstration
|
| Satellite Bus |
|
|
| Launch Mass |
28
kg (62 lbm)
|
| Mission Orbit |
|
|
| Design Life |
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Delta
2 7925-9.5 |
| Launch Date / Time |
29
January 2003
|
18:06
|
| Co-passenger(s) |
NAVSTAR
GPS 2R-8
|
|
FINANCIAL
|
| Satellite cost |
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| Web Links |
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