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

 

 

Table 4-167. Seasat I Characteristics

 

Also called:

Ocean Dynamics Satellite

Date of launch (location):

June 27, 1978 (WTR)

Launch vehicle:

Atlas F

Weight (kg):

2300

Shape:

Two-module spacecraft: cylindrical support bus with two solar paddles; and a roughly cylindrical sensor module with antennas and instruments extending from it

Dimensions (m):

21.0 length

1.5 diameter

Power source:

Solar panels plus NiCd batteries

Responsible NASA center:

Jet Propulsion Laboratory

Prime contractor:

Lockheed Missiles and Space Co.

Project manager:

W. E. Giberson

Objectives:

Demonstrate techniques for global monitoring of oceanographic data for both applications and scientific user; demonstrate key features of an operational ocean dynamics monitoring system.

Instruments:

Scanning Multichannel Microwave Radiometer

Radar Altimeter

Microwave Wand Scatterometer

Synthetic Aperture Imaging Radar

Visible and Infrared Scanning Radiometers

Results:

Successful for 106 days when it lost power on Oct. 10 because of a short in one of the slip-ring assemblies used to connect the rotating solar arrays into the power subsystem. NASA declared the satellite lost on Nov. 21, 1978.

 

Reference: NASA, "Seasat 1 Mission Operations Report," E-655-78-01, June 23, 1978; and U.S. Congress, House of Representatives, Committee on Science and Technology, Subcommittee on Space Science and Applications, SEASAT (Cost, Performance and Schedule Review), Report, 95th Cong., Ist sess. (Washington, 1977).


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