SP-4012 NASA HISTORICAL DATA BOOK: VOLUME III
PROGRAMS AND PROJECTS 1969-1978
 
 

Table 4-83. Nimbus 3 Characteristics

 

Also called:

Nimbus B2

Date of launch (location):

April 14, 1969 (WTR)

Launch vehicle:

Long-Tank Thrust-Augmented Thor (Thorad)-Agena D

Weight (kg):

571

Shape:

butterfly (1.42-meter torus ring base and hexagonal-shaped housing plus two solar paddle wings)

Dimensions (m):

3.05 tall

3.55 wide

1.52 diameter ring

Power source:

Solar panels plus 8 NiCd batteries RTG (SNAP-19)

Responsible NASA center:

GE Company

Project manager:

Harry Press

Project scientist:

William Nordberg

Objectives:

Acquire global samples of infrared spectra from which vertical temperature profiles of the atmosphere may be derived; global mapping of radiative energy balance of Earth atmosphere and cloud cover over one seasonal cycle; demonstrate feasibility of surface pressure and wind measurements with IRLS; global mapping of Earth and its cloud cover (day and night) over a three-month period. Flight test a System for Nuclear Auxiliary Power (SNAP-19), a 50-watt radioactive thermal generator, developed by the Atomic Energy Commission. (Repeat of Nimbus B launch attempt, which failed because of a launch vehicle malfunction in May 1968.)

Equipment:

Medium Infrared (MRIR)

High Resolution Infrared Radiometer (HRIR)

Advanced TV Image Dissector Camera System (IDCS)

Satellite Infrared Spectrometer (SIRS)

Infrared Interferometer Spectrometer (IRIS)

Monitor of Ultraviolet Solar Energy (MUSE)

Interrogation, Recording, and Location System (IRLS)

Results:

Successful; provided daily atmospheric temperature readings up to 30 480 meters; although designed for only 12 months it was operational until March 1972. Launched with SECOR Army satellite.

 

Reference: NASA, "Nimbus 3 Mission Operations Report," S-604-69-04, Apr. 5, 1969.


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