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Molniya-M

Molniya-M

Space Launch Systems
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Basic Information
Name
Molniya-M
Designation
Molniya-M
Alternate Designation
Equipment Type
Space Launch Systems
Manufacturer
Starsem
Date of Introduction
1970
Description

The Molniya launch vehicle is a member of the Soyuz space launch vehicles. The four-stage Molniya-M is the current version of the Molniya launch vehicle and is intended to transport payloads deep into space to the Moon or to the planets of the Solar System. Besides, Molniya-M can place Prognoz and Molniya spacecrafts into high-elliptical near-Earth orbit. The Plesetsk Cosmodrome is entitled for the launch Molniya-M launch vehicles utilizing the same infrastructure in operation for the Soyuz-U launch vehicle. The three-stage rocket uses non-toxic liquid propellant based on oxygen and kerosene. The upper stage (fourth stage) is fueled by cryogenic liquid propellant and ignites an hour after the Molniya-M launch in zero-gravity conditions. The Molniya rocket was retired in 2010.

Air & Air Defense Specifications
Range 40000.0 km
Overview (Deagel)
Group Space Launch Systems
Status Retired - No Longer Operational
Origin Russia
Contractor Starsem
Initial Operational Capability (IOC) 1970
Total Production 221
Specifications (Deagel)
Number of Stages 4
Dimensions — Height 43.4 meter
Dimensions — Rocket Diameter 10.3 meter
Mass — Max Lift-off Weight 309 ton
Mass — Payload to HEO 2,000 kilogram
Percentage — Reliability 98 %
Performance — Orbit 40,000 kilometer
Gear (Deagel)
Item 1 Satellites: Kosmos (1)
Variants
Variant 1 Molniya-M
Variant 2 Soyuz-U
Variant 3 Soyuz-Ikar
Variant 4 Soyuz-Fregat
Variant 5 Soyuz-2
Details
Country of Origin Russia
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
10.3 m
Height
43.4 m
Weight
309000 kg
Operators (1)
Russia
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