MICROSAT 3 (21582)

COSPAR: 1991-051C | Alt Name: Microsat 3
DECAYED

Image
MICROSAT 3 Satellite Image
Additional Sources
Launch Details

Launch Date

July 17, 1991

Launch Site

AFWTR

Launch Pad

RW04/22

Launch Vehicle

Pegasus/HAPS

Orbital Elements

NORAD ID

21582

International Designator

1991-051C

Decay Date

1/24/1992

Basic Satellite Info

Name

MICROSAT 3

Alternative Name

Microsat 3

Type

Payload

Status

Decayed

Owner

DARPA

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
MICROSAT 3, also known as Microsat 3, is an experimental communication satellite launched on July 17, 1991, from AFWTR using a Pegasus/HAPS launch vehicle from Launch Pad RW04/22. The spacecraft has dimensions of 0.2 meters in length and 0.5 meters in both diameter and span. It weighs 21 kg at launch with a dry mass of 19 kg. Equipped with a UHF transponder digital store-and-forward communications system and solar cells with batteries for power, it was designed to operate using cold gas N2 propulsion. The satellite's mission was conducted by DARPA with the purpose of experimental communication. Its design is based on the PicoStar configuration and has a cylindrical shape with an RCS of 0.0689. Manufactured by DSI, MICROSAT 3 had a planned lifetime of four years but achieved only one year in orbit.
Physical Characteristics

Length

0.2

Diameter

0.5

Span

0.5

Dry Mass

19

Launch Mass

21

Shape

Cyl

Radar Cross Section

0.0689

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Microsat 3

Purpose

Experimental communication

Mission

Experimental communication

Manufacturer

DSI

Life Expectancy

4 years (planned); 1 year (achieved)

Bus

Picostar

Configuration

PicoStar

Motor

Cold gas N2 propulsion

Equipment

1 UHF transponder digital store and forward communications system

Power System

Solar cellsm batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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