MOLNIYA 3-43 (22255)

COSPAR: 1992-085A | Alt Name: Molniya-3

DECAYED

Image

Additional Sources

Launch Details

Launch Date

December 2, 1992

Launch Site

PLMSC

Launch Pad

LC43/3

Launch Vehicle

Molniya 8K78M-PVB

Orbital Elements

NORAD ID

22255

International Designator

1992-085A

Decay Date

11/8/2008

Basic Satellite Info

Name

MOLNIYA 3-43

Alternative Name

Molniya-3

Type

Payload

Status

Decayed

Owner

VKS/GPKS

Country

Russia

Constellation

N/A

Related Satellites

Major Events

N/A

Summary

The MOLNIYA 3-43 satellite, also known as Molniya-3, was launched on December 2, 1992, from the Plesetsk Cosmodrome using a Molniya 8K78M-PVB launch vehicle from Launch Pad LC43/3. The satellite is part of the Molniya-3 series and has the configuration KAUR-2. It was manufactured by NPOPM for communication purposes and is owned by VKS/GPKS. With dimensions of 3.6 meters in length, 1.6 meters in diameter, and a span of 8.1 meters, its shape consists of a cylinder with six panels. The satellite's dry mass is 1700 kilograms, and it had an initial launch mass of 1750 kilograms. It is powered by six deployable solar arrays providing up to 1000 watts and includes batteries for power storage. MOLNIYA 3-43 was designed with a motor type KDU-414A (S5.114) or 11D414NS, and its intended operational lifetime was three years.

Physical Characteristics

Length

3.6

Diameter

1.6

Span

8.1

Dry Mass

1700

Launch Mass

1750

Shape

Cyl + 6 Pan

Radar Cross Section

10.9312

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Molniya-3 No. 56

Purpose

Communication

Mission

Communication

Manufacturer

NPOPM

Life Expectancy

3 years

Bus

Molniya-3

Configuration

KAUR-2

Motor

KDU-414A (S5.114) or 11D414NS

Equipment

Unknown

Power System

6 deployable solar arrays (1000 W), batteries

ADCS

Unknown

Transmitter Frequency

Unknown

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