SOYUZ-TMA 2 (27781)

COSPAR: 2003-016A | Alt Name: Soyuz TMA-2
DECAYED

Image
SOYUZ-TMA 2 Satellite Image
Additional Sources
Launch Details

Launch Date

April 26, 2003

Launch Pad

LC1

Launch Vehicle

Soyuz-FG

Orbital Elements

NORAD ID

27781

International Designator

2003-016A

Decay Date

10/28/2003

Basic Satellite Info

Name

SOYUZ-TMA 2

Alternative Name

Soyuz TMA-2

Type

Payload

Status

Decayed

Owner

RKKE

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
Soyuz-TMA 2 (also known as Soyuz TMA-2) is a crewed spacecraft launched by RKKE on April 26, 2003, from the Tyuratam Space Center LC1 launch pad using a Soyuz-FG launch vehicle. The spacecraft has dimensions of 7.9 meters in length and 2.7 meters in diameter with a span of 10.6 meters. It has a dry mass of 2300 kg and a launch mass of 2840 kg. Its configuration includes solar arrays for power generation and batteries, and it is equipped to carry the payload Soyuz 11F732 No. 212. The spacecraft was designed for crewed missions with a shape described as Cyl + Cone + Sphere + 2 Pan. It operates in orbit under Russian ownership (RU) and uses an RCS (Reaction Control System) with a value of 8.0581.
Physical Characteristics

Length

7.9

Diameter

2.7

Span

10.6

Dry Mass

2300

Launch Mass

2840

Shape

Cyl + Cone + Sphere + 2 Pan

Radar Cross Section

8.0581

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Soyuz 11F732 No. 212

Purpose

Crewed spacecraft

Mission

Crewed spacecraft

Manufacturer

RKKE

Life Expectancy

Unknown

Bus

7K-STMA

Configuration

Unknown

Motor

PAO

Equipment

Unknown

Power System

2 deployable fixed solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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