Nimbus 7

Summary

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

Nimbus 7
Artist rendering of the Nimbus 7
Mission typeWeather satellite
OperatorNASA / NOAA
COSPAR ID1978-098A Edit this at Wikidata
SATCAT no.11080
Spacecraft properties
ManufacturerRCA Astrospace
Launch mass965 kilograms (2,127 lb)[1][2]
Dry mass832 kilograms (1,834 lb)
Dimensions3.04 m × 1.52 m × 3.96 m (10.0 ft × 5.0 ft × 13.0 ft)
Power300 W
Start of mission
Launch dateOctober 24, 1978 08:14:01 (1978-10-24UTC08:14:01Z) UTC[3]
RocketDelta-2910 630/D145
Launch siteVandenberg SLC-2W
End of mission
Last contactAugust 1, 1994 (1994-09)[2]
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Eccentricity0.001[1]
Perigee altitude941 kilometers (585 mi)[1]
Apogee altitude954 kilometers (593 mi)[1]
Inclination99.15°[1]
Period104 minutes[1]
Epoch24 October 1978[1]
Last →
 

Launch edit

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 edit

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 edit

Eight experiments were selected, using the following instruments:

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

References edit

  1. ^ a b c d e f g h "Nimbus 7". National Space Science Data Center Master Catalog. NASA Goddard Space Flight Center. Retrieved June 6, 2018.   This article incorporates text from this source, which is in the public domain.
  2. ^ a b "Nimbus 7". WMO OSCAR. World Meteorological Organization. July 28, 2015. Retrieved June 17, 2018.
  3. ^ McDowell, Jonathan C. "GCAT orbital launch log". Jonathan's Space Page. Retrieved November 7, 2023.
  4. ^ Gloersen, P.; Cavalieri, D.J.; et al. (June 30, 1984). "A summary of results from the first NIMBUS 7 SMMR observations". JGR: Atmospheres. 89 (D4): 5335–5344. CiteSeerX 10.1.1.452.4852. doi:10.1029/JD089iD04p05335. (SMMR is mentioned in abstract.)
  5. ^ Stolarski, R.; Krueger, A.; et al. (August 28, 1986). "Nimbus 7 satellite measurements of the springtime Antarctic ozone decrease". Nature. 322 (6082): 808–811. doi:10.1038/322808a0. S2CID 4234789. (SBUV/TOMS are mentioned in abstract.)
  6. ^ "Nimbus 7". NASA Goddard Space Flight Center. Retrieved June 6, 2018.

External links edit

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