Space Shuttle: Difference between revisions

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The [http://ntrs.nasa.gov  NASA technical reports server] supplies a large base of wind tunnel and in-situ performance data of both the mated launch vehicle and the orbiter, and the aerodynamics of the simulated shuttle is based on these documents. The authoritive source for procedures for trajectory management, instrumentation, limits and energency procedures is the [https://www.nasa.gov/centers/johnson/pdf/390651main_shuttle_crew_operations_manual.pdf Space Shuttle Crew Operations Manual] and currently a normal mission, i.e. ascent, orbital insertion, de-orbit, entry, terminal area energy management and landing can be flown largely 'by the book', i.e. following the real procedure for CSS. As of May 2015, this does not yet hold for emergency procedures.
The [http://ntrs.nasa.gov  NASA technical reports server] supplies a large base of wind tunnel and in-situ performance data of both the mated launch vehicle and the orbiter, and the aerodynamics of the simulated shuttle is based on these documents. The authoritive source for procedures for trajectory management, instrumentation, limits and energency procedures is the [https://www.nasa.gov/centers/johnson/pdf/390651main_shuttle_crew_operations_manual.pdf Space Shuttle Crew Operations Manual] and currently a normal mission, i.e. ascent, orbital insertion, de-orbit, entry, terminal area energy management and landing can be flown largely 'by the book', i.e. following the real procedure for CSS. As of May 2015, this does not yet hold for emergency procedures.
== Gallery ==
[[File:Shuttle FG02.jpg|150px| Shuttle Launch]]
[[File:Shuttle_FG03.jpg|150px|Shuttle Launch]]
[[File:Shuttle FG04.jpg|150px| Shuttle Launch]]
[[File:Shuttle launch01.jpg|150px| Launch smoke trail]]
[[File:Shuttle SRBsep03.jpg|150px| SRB separation]]
[[File:Shuttle FG5.jpg|150px| Accelerating to orbital speed]]
[[File:Shuttle Cockpit.jpg|150px|Shuttle 3d cockpit]]
[[File:Shuttle-ETsep01.jpg|150px| External tank separation]]
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