Microsat (SCS)

Launch Partial Failure

Liftoff Time (GMT)

17:33:53

Wednesday July 17, 1991

Mission Details

Launch Notes

The rocket placed the satellites in a lower-than-planned orbit and the spacecraft reentered after 6 months instead of the planned three-year lifetime.

Microsat (SCS)

Wiki

Built by Defense Systems Inc. (DSI) for the Defense Advanced Research Projects Agency (DARPA), the 12-sided Microsats (a.k.a. SCS, Small Communications satellite) measured 10 cm by 48 cm and weighed 22 kg each. They were designed to assess the use of low-earth orbit for global communications. Each satellite operated in UHF, using an analog transponder for FM radio relay of voice communications and a digital transponder to relay data, message, facsimile and modest video traffic. The spacecraft with overlapped footprints provide near continuous communications, which would be global for three planes. The system was intended to provide data for ArcticSat, a system for communicating with nuclear submarines under the polar cap. The microprocessor-controlled digital communications payload was similar to the one used in MACSAT, but with less redundacy and less memory.

Low Earth Orbit

7 Payloads

154 kilograms

Rocket

Retired
Pegasus/HAPS

Active 1991 to 1994

Northrop Grumman logo

Agency

Northrop

Price

$40.00 million

Rocket

Height: 16.9m

Liftoff Thrust

487 Kilonewtons

Fairing

Diameter: 1.15m

Height: 2.13m

Stages

4

Launch Site

NB-52B Carrier

Edwards AFB, California, USA

Fastest Turnaround

75 days 21 hours

Stats

Pegasus


2nd

Mission

1st

Mission of 1991

1991


53rd

Orbital launch attempt