I'm currently working on medium size shuttle system able to achieve 1000km x 1000 km orbit in base configuration.
Whole stack will incorporate following elements:
Orbiter:
Length: 20 m
Wingspan: 18 m
Height 6 m + gear (about 8.5 m)
Crew: 2
Passengers: 2 (+6 in SBUS module)
Cargo capacity: ~4 mT (without SBUS module)
Airlocks: 2 - one on the nosecone , one in cago bay (Second airlock is used either to connect passenger module a.k.a SBUS or to perform EVA, Nosecone airlock may be used as docking port or to perform EVA)
There are few modules for this Orbiter in devolopement such as:
SBUS: can carry up to 6 passengers with additional LSS
Spyglass: 2.6 m wide optical telescope with adaptive optics
HOFS (high orbit fuel system): additional 3.8 mT of fuel to reach higher orbits.
Some shuttle shots:
launcher and other spcs in 2-3 days.
Whole stack will incorporate following elements:
Orbiter:
Length: 20 m
Wingspan: 18 m
Height 6 m + gear (about 8.5 m)
Crew: 2
Passengers: 2 (+6 in SBUS module)
Cargo capacity: ~4 mT (without SBUS module)
Airlocks: 2 - one on the nosecone , one in cago bay (Second airlock is used either to connect passenger module a.k.a SBUS or to perform EVA, Nosecone airlock may be used as docking port or to perform EVA)
There are few modules for this Orbiter in devolopement such as:
SBUS: can carry up to 6 passengers with additional LSS
Spyglass: 2.6 m wide optical telescope with adaptive optics
HOFS (high orbit fuel system): additional 3.8 mT of fuel to reach higher orbits.
Some shuttle shots:
launcher and other spcs in 2-3 days.
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