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European - HOTOL space shuttle


Interim HOTOL
spacecraft

Hotol Interim HOTOL
(Horizontal Take-Off and Landing)

* Developer:
British Aerospace Dr.Bob Parkinson
* Payload:
?? kg

to 200 km Orbit

- Payload bay ?? m x ?? m x ?? m
- Total Habitable Volume: ca. 1,211.00 m3
* Chronology:
- Start Development : 1991
* upper Stage:
- Engine: 11D122
- Number of Engines: 4
- Total Thrust (vac): 4 x 2.000 kN
- Propellants: LH2 / LOX / Kerosene
* Crew:
- crew: ??
* Spacecraft:
- Total Mass (max): 250.000 kg
- Empty Mass: 33.100 kg
- Length over all: 36.45 m
- max.Hight: 8.60 m
- wing Span: 21.60 m
- fuselage max. diameter: 6.10 m

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HOTOL - AN-225
air launch vehicle

Launch vehicle: AN-225 MRIYA

AN-225/HOTOL

AN-225 / HOTOL

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