PROGRESS-M 5 (20824)

COSPAR: 1990-085A | Alt Name: Progress M-5
DECAYED

Image
PROGRESS-M 5 Satellite Image
Additional Sources
Launch Details

Launch Date

September 27, 1990

Launch Pad

LC1

Launch Vehicle

Soyuz-U2

Orbital Elements

NORAD ID

20824

International Designator

1990-085A

Decay Date

11/28/1990

Basic Satellite Info

Name

PROGRESS-M 5

Alternative Name

Progress M-5

Type

Payload

Status

Decayed

Owner

NPOE

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
PROGRESS-M 5 (also known as Progress M-5) is a cargo satellite manufactured by NPOE and was launched on September 27, 1990, from the Tyuratam Space Center using the Soyuz-U2 launch vehicle. The spacecraft has dimensions of 7.9 meters in length and diameter with a span also measuring 7.9 meters. It had a dry mass of 4500 kg and launched with a total mass of 7320 kg. PROGRESS-M 5 was equipped with two deployable fixed solar arrays and batteries for power supply, and its propulsion system used the KTDU-80 (S5.80) motor. The mission purpose was to transport cargo, and it featured a shape described as a sphere combined with cone, cylinder, and pan elements.
Physical Characteristics

Length

7.9

Diameter

2.7

Span

7.9

Dry Mass

4500

Launch Mass

7320

Shape

Sphere + Cone + Cyl + Pan

Radar Cross Section

180.98

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Progress 7K-TGM No. 206

Purpose

Cargo

Mission

Cargo

Manufacturer

NPOE

Life Expectancy

Unknown

Bus

7K-TGM

Configuration

Unknown

Motor

KTDU-80 (S5.80)

Equipment

Unknown

Power System

2 deployable fixed solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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