Difference between revisions of "Shuttle PB"
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its hover thrusters for takeoff and landing. Aerodynamic control surfaces are not supported in | 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). | this version. Attitude control is performed via the RCS (reaction control system). | ||
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| + | <gallery widths="200" heights="200"> | ||
| + | ShuttlePB-Orbiter2005P1.jpg|<center>Shuttle PB in Orbiter 2005P1</center> | ||
| + | </gallery> | ||
[[Category: Articles]] | [[Category: Articles]] | ||
{{stub}} | {{stub}} | ||
Revision as of 13:07, 16 September 2024
The 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).
Shuttle PB in Orbiter 2005P1
