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Courier 1A

NSSDCA ID: COUR1A
COSPAR ID: 

Description

Courier 1A was an experimental military communications satellite that was launched from Cape Canaveral. The mission failed after 2 1/2 minutes of flight when the first stage exploded. Run by the U.S. Army Advanced Research Project Agency, Courier was a successor to the SCORE program. The objective of the mission was to put the satellite into a 1000 km (600 mile) altitude Earth orbit and test the feasibility of a global military communications network using "delayed repeater" satellites, which receive and store information until commanded to transmit.

Spacecraft and Subsystems

Courier 1A was a 225 kg (500 lb.), 129.5 cm (51 in.) diameter sphere, 135 kg (300 lb.) of this was the electronic equipment payload. It carried four 2-W microwave FM (1700-1800 MHz) tranmitters and a 50-mW transistorized VHF beacon transmitter subsystem. It contained four solid-state receivers in the 1800-1900 MHz microwave band. Five tape recorders were used to store data for later playback. Four of these were digital with a total capacity of 13.2 Mb (4 minutes at 55 kbps) each. One was an analog recorder with 4 minute capacity and a range of 300 to 50,000 Hz. Four whip antennas were mounted at 90 degree intervals along the equator of the sphere. It also held two microwave antennas, a transistorized telemetry generator, VHF diplexer, and a command decoder. The transmitters and receivers were set up so two of each would be running at any given time, the others were on standby and could be switched in by ground command. The sphere was covered with 19,200 solar cells, charging nickel-cadmium batteries, providing 60 W power. The satellite had the capability to simultaneously transmit, receive, and store approximately 68,000 coded words per minute. It also had real-time communications mode, supporting a single half-duplex voice circuit.

Mission Profile

Courier 1A launched on 18 August 1960 at 19:58 UT (3:58 p.m. EDT) from the Atlantic Missile Range in Cape Canaveral, Florida. The launch vehicle was a Thor-Able-Star, comprising a modified USAF Thor IRBM first stage and a USAF Able-Star upper stage with a re-startable liquid engine. Approximately 150 seconds after launch the first stage cut off prematurely, resulting in an explosion and failure of the mission.

Alternate Names

    Facts in Brief

    Launch Date: 1960-08-18
    Launch Vehicle: Thor-Able-Star
    Launch Site: Cape Canaveral, United States
    Mass: 225 kg
    Nominal Power: 60 W

    Funding Agency

    • Department of Defense-Department of the Air Force (United States)

    Discipline

    • Communications

    Additional Information

    Questions and comments about this spacecraft can be directed to: Dr. David R. Williams

     

    Personnel

    NameRoleOriginal AffiliationE-mail
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