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

 

Table 3-127. Voyager I Characteristics

 

Also called:

Voyager Jupiter-Saturn

Date of launch (location):

Sept. 5, 1977 (ETR)

Launch vehicle:

Titan-Centaur

Weight (kg):

822, mission module

1211, propulsion module

47, spacecraft adapter

2080, total

Shape:

10-sided main structure, with a 3.66-m diameter parabolic reflector supporter above the spacecraft body

Dimensions (m):

4.70 height

1.78 from flat to flat

2.30 science boom

Power source:

3 RTGs

Responsible NASA center:

JPL

Project manager:

John R. Casani

Science Manager:

James E. Long

Objectives:

To conduct comparative studies of the Jupiter and Saturn planetary systems, including their satellites and Saturn's rings; study the interplanetary medium between earth and Saturn.

Experiments (responsible institution):

.

.

Imaging science (University of Arizona)

Infrared spectroscopy interferometer and radiometry (GSFC)

Ultraviolet spectroscopy (Kitt Peak National Observatory)

Photopolarimetry (University of Colorado)

Plasma (Massachusetts Institute of Technology)

Low-energy charged particles (Johns Hopkins Applied Physics Laboratory)

Magnetic fields (GSFC)

Planetary radio astronomy (University of Colorado)

Plasma wave (TRW Space and Defense Systems)

Radio science (Stanford University)

Results:

Successful; reached vicinity of Jupiter on March 5, 1979 and Saturn on November 12, 1980; returned much new information on both planets.

 

Reference: JPL, "Voyager Jupiter-Saturn Fact Sheet," Dec. 1976.


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