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

Table 4-94. Anik 3 Characteristics

 

Also called:

Telesat-C; Anik A-3

Date of launch (location):

May 7, 1975 (ETR)

Launch vehicle:

Delta 2914

Weight (kg):

270

Shape:

cylindrical with a parabolic mesh antenna extending from one end

Dimensions (m):

1.8 diameter

3.3 height

Power source:

Solar cells plus NiCd batteries

NASA's role:

Launch vehicle and support (reimbursable)

Cooperating organizations:

NASA and Telesat of Canada

Prime contractor:

Hughes Aircraft Company

Responsible NASA center:

Goddard Space Flight Center

Project manager:

Robert J. Goss

Objectives:

Provide transmission of TV, voice, data, etc., (analog or digital signals) throughout Canada for seven years.

Results:

Successful; third and last of "A" series.

 

Reference: NASA, "Anik 3 Mission Operations Report," S-492-201-75-03, Apr. 25, 1975.

 


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