Nimbus 7

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Nimbus 7
Nimbus rendering.jpg
Artist rendering of the Nimbus 7
Mission type Weather satellite
Operator NASA  / NOAA
COSPAR ID 1978-098A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 11080
Spacecraft properties
Manufacturer RCA 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]
Rocket Delta-2910 630/D145
Launch site Vandenberg SLC-2W
End of mission
Last contactAugust 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 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.

Contents

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:

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

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References

  1. 1 2 3 4 5 6 7 8 "Nimbus 7". National Space Science Data Center Master Catalog. NASA Goddard Space Flight Center. Retrieved June 6, 2018.PD-icon.svg This article incorporates text from this source, which is in the public domain.
  2. 1 2 "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.