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Technical Specifications
The Applications Technology Satellite (ATS) series
was a set of six NASA spacecraft launched from Dec. 7, 1966, to
May 30, 1974, to flight-test and demonstrate new technologies and
techniques for communications, meteorological and navigation
satellites. ATS was a multi-purpose engineering satellite series,
testing technology in communications and meteorology from
geosynchronous orbit. The major objective of the early ATS
satellites was to test whether gravity would anchor the satellite
in a synchronous orbit (22,300 statute miles above the Earth),
allowing it to move at the same rate the Earth is turning, thus
seeming to remain stationary.
Although the ATS satellites were intended mainly as test
beds, they did collect and transmit meteorological data and
functioned at times as communications satellites. ATS provided the
first color images from space as well as regular cloud cover
images for meteorological studies.
ATS Application Technology Satellites |
| PAYLOAD
CAPABILITIES |
| Types of Services |
Technology
demonstration |
| Downlink frequencies |
|
| CORE BUS
SPECIFICATIONS |
| Prime Contractor |
|
| Platform |
-
|
| Launch Mass |
|
| Design Life |
|
STRUCTURE |
| Dimensions (H x W x L) |
|
| Construction |
|
POWER SYSTEM |
| Payload Power
(EOL) |
|
| Solar Arrays |
|
| Batteries |
|
ATTITUDE CONTROL SYSTEM |
| Stabilization |
|
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