Difference between revisions of "Shuttle-PB"

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m (Reverted edits by UrwumpeFUCKERS (Talk); changed back to last version by Urwumpe)
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{{Infobox Vessel|name=Shuttle-PB
 
{{Infobox Vessel|name=Shuttle-PB
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|pic1_text=Shuttle-PB
 
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|full_name=Shuttle-PB

Revision as of 00:24, 10 December 2012

Shuttle-PB
Shuttle PB.jpg
Shuttle-PB
Description
Role Single-crew exploratory vehicle
Full name Shuttle-PB
Crew 1
Passengers none
First flight date unknown
Entered service date unknown
Manufacturer unknown
Dimensions
Length 6.8 m
Height 5.2 m
Wingspan 2.4 m
Wing area
Masses
Empty 500 kg
Fuel 750 kg
RCS fuel n/a
Max. take-off 1,250 kg
Inertia PMI - m2
Performance
Max. delta-v 45.8 km/s
Max. accel 60 m/s2
Stall CL
Stall AOA

The Shuttle-PB is a very agile single-seater. It produces little lift in atmospheric flight, and depends on its hover thrusters for takeoff and landing. Aerodynamic control surfaces are not supported in this version. Attitude control is performed via the RCS (reaction control system).

The Shuttle-PB has been somewhat neglected in recent versions of Orbiter; it has only a basic aerodynamic model and no instrument panel or animations, it is not capable of horizontal takeoff or landing and it has no retro engine.