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Russian - MAKS-OS space shuttle

MAKS - OS
spacecraft

mmaks.gif (9072 Byte) MAKS-OS
(Multipurpose Aerospace System)

* Developer:
NPO Molniya Bureau
* Payload:
8,300 kg

to 200 km Orbit
- Payload bay 2.60 m x 6.80 m
- Total Habitable Volume: 46.00 m3
* Chronology:
- Start Development : ca. 1980
* upper Stage:
- Engine: RD-701
- Number of Engines: 2
- Total Thrust (vac): 2 x 2.000 kN
- Propellants: LH2 / LOX / Kerosene
* Crew:
- crew: 2
- passenger in (pressurized cabin): 4
* Spacecraft:
- Total Mass (max): 27,000 kg
- Empty Mass: 18.000 kg
- Length over all: 19.30 m
- max.Hight: 6.80 m
- wing Span: 12.50 m
- fuselage max. diameter: 2.60 - 3.00 m

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MAKS - OS - tank
external tank

Maks with external fuel tank
MAKS-OS-Tank

* Developer:
NPO Molniya Bureau
* Chronology:
- Start Development : ca. 1980
* Fuel Tank:
- Total Mass (max): 248,000 kg
- Empty Mass: 11.000 kg
- Length over all: 32.80 m
- Length with the spacecraft: 36.30 m
- max. Diameter: 6.80 m

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MAKS - OS - AN-225
air launch vehicle

Launch vehicle:AN-225 MRIYA

AN-225/MAKS

AN-225 / MAKS

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