SOYUZ-TM 13 (21735)

COSPAR: 1991-069A | Alt Name: Soyuz TM-13
DECAYED

Image
SOYUZ-TM 13 Satellite Image
Additional Sources
Launch Details

Launch Date

October 2, 1991

Launch Pad

LC1

Launch Vehicle

Soyuz-U2

Orbital Elements

NORAD ID

21735

International Designator

1991-069A

Decay Date

3/25/1992

Basic Satellite Info

Name

SOYUZ-TM 13

Alternative Name

Soyuz TM-13

Type

Payload

Status

Decayed

Owner

NPOE

Country

USSR

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
SOYUZ-TM 13 was a crewed spacecraft launched by NPOE on October 2, 1991, from Tyuratam Site (TYMSC) using the Soyuz-U2 launch vehicle from Launch Pad LC1. It has dimensions of 7.2 meters in length and 2.2 meters in diameter with a span of 10.6 meters. The spacecraft had a dry mass of 2850 kg, which is also its launch mass. Equipped with two deployable fixed solar arrays and batteries for power generation, the spacecraft featured a shape described as Sphere + Cone + Cyl + 2 Pan. Its mission was to serve as a crewed spacecraft. The launch date stabilized on October 2, 1991, at 06:08:29. The Soyuz-TM 13's propulsion system included the KTDU-80 (S5.80) motor and an RCS of 19.17. Manufactured by NPOE in SU (former Soviet Union), its payload was designated as Soyuz 7K-STM No. 63, with a configuration not specified and no additional equipment details provided.
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

19.17

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Soyuz 7K-STM No. 63

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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