SOYUZ-TM 5 (19204)

COSPAR: 1988-048A | Alt Name: Soyuz TM-5
DECAYED

Image
SOYUZ-TM 5 Satellite Image
Additional Sources
Launch Details

Launch Date

June 7, 1988

Launch Pad

LC1

Launch Vehicle

Soyuz-U2

Orbital Elements

NORAD ID

19204

International Designator

1988-048A

Decay Date

9/7/1988

Basic Satellite Info

Name

SOYUZ-TM 5

Alternative Name

Soyuz TM-5

Type

Payload

Status

Decayed

Owner

NPOE

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
SOYUZ-TM 5, also known as Soyuz TM-5, is a crewed spacecraft launched on June 7, 1988, from the TYSMC launch site using the Soyuz-U2 launch vehicle. The spacecraft has dimensions of 7.2 meters in length, 2.2 meters in diameter, and spans 10.6 meters. It was manufactured by NPOE with a dry mass of 2850 kg and launched at the same mass. SOYUZ-TM 5 is equipped with two deployable fixed solar arrays and batteries for power supply. The spacecraft's shape consists of a sphere, cone, cylinder, and two panels. Its mission purpose was to serve as a crewed spacecraft, utilizing the KTDU-80 (S5.80) motor. It stabilized in orbit on June 7, 1988, at 1412:01 UTC, marking its operational start.
Physical Characteristics

Length

7.2

Diameter

2.2

Span

10.6

Dry Mass

2850

Launch Mass

2850

Shape

Sphere + Cone + Cyl + 2 Pan

Radar Cross Section

335.09

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Soyuz 7K-STM No. 55

Purpose

Crewed spacecraft

Mission

Crewed spacecraft

Manufacturer

NPOE

Life Expectancy

Unknown

Bus

7K-STM

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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