RME (USA 52) (20497)

COSPAR: 1990-015B | Alt Name: RME

DECAYED

Image

Additional Sources

Launch Details

Launch Date

February 14, 1990

Launch Site

Cape Canaveral Space Force Station

Launch Pad

LC17B

Launch Vehicle

Delta 6920-8

Orbital Elements

NORAD ID

20497

International Designator

1990-015B

Decay Date

5/24/1992

Basic Satellite Info

Name

RME (USA 52)

Alternative Name

RME

Type

Payload

Status

Decayed

Owner

SDIO

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Summary

RME (USA 52), identified by NORAD_CAT_ID 20497 and OBJECT_ID 1990-015B, is a satellite manufactured by BALL for the SDIO under the mission of conducting SDI experiments. Launched on February 14, 1990, from Launch Pad LC17B at AFETR using the Delta 6920-8 launch vehicle, RME has dimensions of 1.6 meters in length, diameter, and span with a dry mass of 1000 kg. The satellite is powered by solar cells and batteries and features a dodecahedral cylindrical shape with a radar cross-section (RCS) of 4.28 square meters. RME's purpose aligns with its mission to conduct SDI experiments, though specific details on its configuration, equipment, motor type, and other specifications are not provided.

Physical Characteristics

Length

1.6

Diameter

1.6

Span

1.6

Dry Mass

1000

Launch Mass

1000

Shape

Dodec Cyl

Radar Cross Section

4.28

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

RME

Purpose

SDI Experiments

Mission

SDI Experiments

Manufacturer

BALL

Life Expectancy

Unknown

Bus

RME

Configuration

Unknown

Motor

Equipment

Unknown

Power System

Solar cells, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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