SOYUZ-TM 17 (22704)

COSPAR: 1993-043A | Alt Name: Soyuz TM-17
DECAYED

Image
SOYUZ-TM 17 Satellite Image
Additional Sources
Launch Details

Launch Date

July 1, 1993

Launch Pad

LC1

Launch Vehicle

Soyuz-U2

Orbital Elements

NORAD ID

22704

International Designator

1993-043A

Decay Date

1/14/1994

Basic Satellite Info

Name

SOYUZ-TM 17

Alternative Name

Soyuz TM-17

Type

Payload

Status

Decayed

Owner

NPOE

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Summary
SOYUZ-TM 17, also known as Soyuz TM-17, is a crewed spacecraft launched on July 1, 1993, from the Tyuratam Space Center Launch Site (TYMSC) using the Soyuz-U2 launch vehicle from LC1. The satellite has dimensions of 7.2 meters in length and 2.2 meters in diameter with a span of 10.6 meters. It was manufactured by NPOE and carries the Soyuz 7K-STM No. 66 payload. SOYUZ-TM 17 is powered by two deployable fixed solar arrays and batteries, and its shape consists of a sphere plus cone plus cylinder with two panels. The spacecraft has a dry mass and launch mass both at 2850 kilograms and is equipped with the KTDU-80 (S5.80) motor for propulsion. Its RCS value is 0.31. This satellite was launched as part of Russia's efforts to maintain crewed missions, with no specific lifetime defined in the provided data.
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

0.31

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Soyuz 7K-STM No. 66

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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