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The 100 kg (220 lbm) STRV 1C
satellite will be placed in a 590 km by 39,248 km orbit, with an
inclination of 6.5 degrees to the equator. After spacecraft
separation, the spacecraft will do no maneuvering. The cubic craft
will spin at around 10 degrees per second, enough to keep the
satellite stable. The satellite is designed to operate for 1 year.
The satellite is expected to have 80 watts of power at the
beginning of their life. The stowed dimensions of each satellite
are .7 m x .7 m x .7 m.
The two STRV spacecraft will test a
series of new systems and theories. The STRV satellites will be
the first satellites to operate using a lithium ion battery, will
test a new secure communications system, will demonstrate a new
Internet-based communications system, and will be the first
satellites to evaluate the signal from GPS satellites from a
higher orbit.
The United Kingdom Defence
Evaluation and Research Agency (DERA) built and operates the two
satellites. Additional
sponsors of the mission include the United Kingdom Ministry of
Defense, the United States Ballistic Missile Defense Organization,
the United States Air Force, ESA, and Canada.
| STRV
1C
|
|
SATELLITE
|
| Int'l Designation |
2000
072B
|
launched
|
| Owner / Sponsor |
United
Kingdom Defence Evaluation and Research Agency (DERA)
|
| Mission |
Engineering
Demonstration
|
| Satellite Bus |
custom
|
| Launch Mass |
100
kg
(220 lbm)
|
| Mission Orbit |
EEO -
590 km x 39,248 km
|
6.5°
|
| Design Life |
1
year
|
| Power (BOL) |
0.800
kW
|
|
LAUNCH
|
| Launch Vehicle
Model |
Ariane
5 |
| Date / Time (UTC) |
2000
Nov 16
|
01:07
|
|
CO-PASSENGER(S)
|
| Name(s) |
PAS
1R
|
| |
AMSAT
Oscar 40
|
| |
STRV
1D
|
|
FINANCIAL
|
| Satellite cost |
|
| Web Links |
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