| Nimbus 5 | |
| Mission Type: | Weather satellite |
| Manufacturer: | RCA Astrospace |
| Launch Mass: | 770kg (1,700lb) |
| Dimensions: | tall x dia. |
| Launch Date: | UTC[1] |
| Launch Rocket: | Delta-900 577/D93 |
| Launch Site: | Vandenberg SLC-2W |
| Last Contact: | [2] |
| Orbit Reference: | Geocentric |
| Orbit Regime: | Low Earth |
| Orbit Eccentricity: | 0.0008 |
| Orbit Periapsis: | 1089km (677miles) |
| Orbit Apoapsis: | 1101km (684miles) |
| Orbit Inclination: | 99° |
| Orbit Period: | 107.2 minutes |
| Apsis: | gee |
| Programme: | Nimbus program |
| Previous Mission: | Nimbus 4 |
| Next Mission: | Nimbus 6 |
Nimbus 5 (also called Nimbus E or Nimbus V) was a meteorological satellite for the research and development of sensing technology. It was the fifth successful launch in a series of the Nimbus program.
The objective of Nimbus 5 was to test and evaluate advanced sensing technology, and to provide improved photographs of cloud formations.[3]
Nimbus 5 was launched on December 11, 1972, by a Delta rocket from Vandenberg Air Force Base, California, USA. The satellite orbited the Earth once every 107 minutes, at an inclination of 99°. Its perigee was 1089km (677miles) and its apogee was 1101km (684miles).
There were six science instruments aboard Nimbus 5. The satellite also included Sun sensors, and horizon scanners for navigation.
The ITPR was designed to obtain vertical profiles of temperature and moisture in the atmosphere. A 3-dimensional map could then be created with a resolution of .[4]
The SCR had three objectives: to observe the global atmospheric temperature structure, to observe the distribution of water vapor, and to measure the density of ice crystals in cirrus clouds. Its sensing resolution was about .[5]
NEMS was used to demonstrate the use of microwave sensors for measuring tropospheric temperature profiles, water content in clouds, and surface temperature. The instrument monitored five selected frequencies continuously. The data were recorded on a magnetic tape so they could be transmitted later.[6]
See main article: Electrically scanning microwave radiometer. ESMR was used for mapping the microwave radiation from Earth's surface. This information was used to measure the water content of clouds, and to observe sea ice. It was also used to test the use of microwaves to measure soil moisture. The antenna system was deployed after launch, and controlled by an onboard computer.[7]
For measuring the thermal emission characteristics of Earth's surface and sea temperatures. A scanning mirror rotated ten times per second to sense sections wide. SCMR malfunctioned soon after launch.[8]
THIR was used for measuring cloud top temperatures and water vapor content in the stratosphere. It could measure cloud temperatures in the day and at night. The sensing unit was a bolometer made from germanium.[9]