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

 

Table 3-115. Mariner 6 Characteristics

 

Also called:

Mariner Mars 69

Date of launch (range):

Feb. 24, 1969 (ETR)

Launch vehicle:

Atlas-Centaur

Shape:

octagonal with 4 solar panels

Weight (kg):

381

Dimensions (m):

1.37, width; 5.79 with panels extended

0.46, height; 3.35 with panels extended

Power source:

solar panels plus AgZn battery

Prime contractor:

in-house

Date of reentry:

N/A Heliocentric orbit

Responsible NASA center:

JPL

Project manager:

H. M. Schurmeier

Project scientist:

J. A. Stallkamp

Objectives:

To conduct flyby missions in order to make exploratory investigations of Mars. Information sought regarding Martian topography and atmosphere in the equatorial region (Mariner 7 twin mission).

Experiments (responsible organization):

.

television (California Institute of Technology)

infrared spectrometer (Univ. of California at Berkeley)

ultraviolet spectrometer (Univ. of Colorado)

infrared radiometer (CIT)

celestial mechanics (JPL)

S-band occultation (JPL)

Results:

Successful; passed by Mars on July 31, 1969, within 3200 kilometers. Together Mariner 6 and 7 returned a total of 200 television pictures of the planet; the probes were used in 1970 in an experiment to verify the theory of relativity.

 

Reference: MOR S-816-69-01/02, Feb. 18, 1969; and NASA Hq., "Mission Report, Mariners Six and Seven," Oct. 29, 1969.

 


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