NSSDCA/COSPAR ID: 1976-004A
This three-axis stabilized satellite was designed as a test vehicle to carry communications-related equipment. The purpose of its launch into an equatorial, earth-synchronous orbit was -- (1) to demonstrate new technology, (2) to conduct communications technological experiments, and (3) to develop new communications methodology in conjunction with ground-based components. The spacecraft was a short (1.17-m) right cylinder (1.8-m diameter) with two parallel (1.72-m apart) plane surfaces symmetrically truncating the curved surface. These plane surfaces were also parallel to the cylinder axis. Relatively long, narrow (1.3- by 6.5-m) solar arrays were extendable from mechanisms mounted on the parallel plane sides. A more complete description may be found in the 'NASA-GSFC Mission Operation Plan, section 1,' and in the Mission Operation Report.
Launch Date: 1976-01-17
Launch Vehicle: Delta
Launch Site: Cape Canaveral, United States
Mass: 680 kg
Questions and comments about this spacecraft can be directed to: Coordinated Request and User Support Office
Name | Role | Original Affiliation | |
---|---|---|---|
Dr. Wasyl M. Lew, Jr. | Program Manager | NASA Headquarters | |
Dr. J. N. Barry | Project Manager | Department of Communications/Communications Research Centre | |
Dr. Irvine Paghis | Program Manager | Department of Communications/Communications Research Centre | |
Dr. A. S. Brown | Project Scientist | Department of Communications/Communications Research Centre |