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

 

Table 4-101. CTS-1 Characteristics

 

Also called:

Communications Technology Satellite

Date of launch (location):

Jan. 17, 1976 (ETR)

Launch vehicle:

Delta 2914

Weight (kg):

676.8

Shape:

Roughly cylindrical with solar panels

Dimensions (m):

1.88 height (16.5 with solar panels extended)

1.83 diameter

Power source:

Solar cells plus NiCd batteries

NASA's role:

Launch vehicle, spacecraft testing, instruments (traveling wave tube)

Cooperating organizations:

NASA and Canadian Department of Communications

Spacecraft provider:

Canadian Communications Research Center

Responsible NASA center:

Goddard Space Flight Center

Lewis Research Center

Mission operations managers:

William H. Robbins: Robert G. Sanford

Objectives:

To advance the technology of spacecraft-mounted and related ground-based components applicable to high-radiated RF-power satellites; two year experiment program.

U.S. experiments:

Transmitter Experiment Package

Solar Array Technology Experiment

Attitude Control System Experiment

Biomedical Communications

Health Communications

Communications Support for Decentralized Medical Education

Health Educational Television

College Curriculum Sharing

Project Interchange

Satellite Distribution Experiment

Communications in Lieu of Transportation

Transportable Emergency Earth Terminal

Interactive Techniques for Intra-NASA Applications

Communications Link Characterization

12 GHz Low-Cost Receivers

Results:

Successful; most powerful communications satellite launched to that date; operations ceased in Oct. 1979.

Reference: NASA, "CTS Mission Operations Report," E-610-76-01, Dec. 30, 1975.

 


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