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

Table 4-93. Anik 2 Characteristics

 

Also called:

Telesat-B; Anik A-2

Date of launch (location):

Apr. 20, 1973 (ETR)

Launch vehicle:

Delta 1914

Weight (kg):

273

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; second in series.

 

Reference: NASA, "Anik 2 Mission Operations Report," S-492-201-73-02, Mar. 7, 1973.


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