PROGRESS-M 14 (22090)

COSPAR: 1992-055A | Alt Name: Progress M-14

DECAYED

Image

Additional Sources

Launch Details

Launch Date

August 15, 1992

Launch Site

Tyuratam Missile and Space Complex

Launch Pad

LC31

Launch Vehicle

Soyuz-U2

Orbital Elements

NORAD ID

22090

International Designator

1992-055A

Decay Date

10/21/1992

Basic Satellite Info

Name

PROGRESS-M 14

Alternative Name

Progress M-14

Type

Payload

Status

Decayed

Owner

NPOE

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Summary

The PROGRESS-M 14 satellite, also known as Progress M-14, was launched on August 15, 1992, from the TSYMC launch site using a Soyuz-U2 launch vehicle from launch pad LC31. It has a bus type of 7K-TGM and is used for cargo missions. The satellite measures 7.9 meters in length with a diameter of 2.7 meters and a span of 7.9 meters, weighing 6426 kg at launch and having a dry mass of 3750 kg. It was manufactured by NPOE and its motor is the KTDU-80 (S5.80). The satellite's power system includes two deployable fixed solar arrays and batteries. Its shape consists of a sphere, cone, cylinder, and pan. The purpose of this satellite is to deliver cargo to space stations or other orbital destinations.

Physical Characteristics

Length

7.9

Diameter

2.7

Span

7.9

Dry Mass

3750

Launch Mass

6426

Shape

Sphere + Cone + Cyl + Pan

Radar Cross Section

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Progress 7K-TGM No. 209

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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