Nimbus 7

Nimbus 7

Artist rendering of the Nimbus 7
Mission type	Weather satellite
Operator	NASA / NOAA
COSPAR ID	1978-098A
SATCAT no.	11080
Spacecraft properties
Manufacturer	RCA Astrospace
Launch mass	965 kilograms (2,127 lb)[1][2]
Dry mass	832 kilograms (1,834 lb)
Dimensions	3.04 m × 1.52 m × 3.96 m (10.0 ft × 5.0 ft × 13.0 ft)
Power	300 W
Start of mission
Launch date	October 24, 1978 08:14:01 (1978-10-24UTC08:14:01Z) UTC[3]
Rocket	Delta-2910 630/D145
Launch site	Vandenberg SLC-2W
End of mission
Last contact	August 1, 1994 (1994-09)[2]
Orbital parameters
Reference system	Geocentric
Regime	Low Earth
Eccentricity	0.001[1]
Perigee altitude	941 kilometers (585 mi)[1]
Apogee altitude	954 kilometers (593 mi)[1]
Inclination	99.15°[1]
Period	104 minutes[1]
Epoch	24 October 1978[1]
Nimbus program ← Nimbus 6 Last →

Nimbus 7 (also called Nimbus G) was a meteorological satellite. It was the seventh and last in a series of the Nimbus program.

Launch

Nimbus 7 was launched on October 24, 1978, by a Delta rocket from Vandenberg Air Force Base, California, United States. The spacecraft functioned nominally until 1994. The satellite orbited the Earth once every 1 hour and 34 minutes, at an inclination of 99 degrees. Its perigee was 941 kilometers (585 mi) and its apogee was 954 kilometers (593 mi).^[1]

Mission

The Nimbus 7 research and development satellite served as a stabilized, Earth-oriented platform for the testing of advanced systems for sensing and collecting data in the pollution, oceanographic, and meteorological disciplines. The polar-orbiting spacecraft consisted of three major structures: a hollow torus-shaped sensor mount, solar paddles, and a control housing unit that was connected to the sensor mount by a tripod truss structure.

Configured somewhat like an ocean buoy, Nimbus 7 was nearly 3.04 metres (10.0 ft) tall, 1.52 metres (5.0 ft) in diameter at the base, and about 3.96 metres (13.0 ft) wide with solar paddles extended. The electronics equipment and battery modules were housed in the sensor mount (torus) that formed the satellite base. The lower surface of the torus provided mounting space for sensors and antennas. A box-beam structure mounted within the center of the torus provided support for the larger sensor experiments. Mounted on the control housing unit, which was located on top of the spacecraft, were Sun sensors, horizon scanners, and a command antenna. The spacecraft's spin axis was pointed at the Earth. An advanced attitude-control system permitted the spacecraft's orientation to be controlled to within plus or minus 1 degree in all three axes (pitch, roll, yaw).

Instruments

Eight experiments were selected, using the following instruments:

• Coastal-Zone Color Scanner (CZCS)
• Earth Radiation Budget (ERB)
• Limb Infrared Monitoring of the Stratosphere (LIMS)
• Scanning Multichannel Microwave Radiometer (SMMR)^[4]
• Solar Backscatter UV and Total Ozone Mapping Spectrometer (SBUV/TOMS)^[5]
• Stratospheric Aerosol Measurement II (SAM II)
• Stratospheric and Mesospheric Sounder (SAMS)
• Temperature-Humidity Infrared Radiometer (THIR)

These sensors were capable of observing several parameters at and below the mesospheric levels.^[6]

References

External links

• Live Real Time Satellite Tracking and Predictions: Nimbus 7 N2YO.com