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

Table 4-136. OTS 1 Characteristics

 

Also called:

Orbital Test Satellite; Operations Technology Satellite

Date of launch (location):

Sept. 13, 1977 (ETR)

Launch vehicle:

Delta 3914

Weight (kg):

865

Shape:

Six-sided with two solar panels

Dimensions (m):

2.13 length (9.26 with solar array deployed)

2.39 height

Power source:

Solar panels and NiCd battery

NASA's role:

Launch vehicle (reimbursable)

Cooperating organizations:

NASA and European Space Agency

Prime contractor:

Hawker Siddeley Dynamics

Objectives:

Three-year commercial communications system for Europe; capable of 6000 telephone circuits.

Results:

Unsuccessful; Castor IV strap-on motor malfunctioned during launch; vehicle exploded 54 seconds after liftoff.

 

Reference: ESA, "ESA's OTS-2 Communications Satellite Due to Launch End April," ESA news release, Apr. 7, 1978; and NASA, "OTS I Mission Operations Report," M-492-210-77-01, Sept. 8, 1977.


-
Back -