First Sentence:
The problems associated with determining the aerothermodynamic environment of a vehicle flying through the atmosphere offer diverse challenges to the designer.
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Key Phrases - Statistically Improbable Phrases (SIPs):
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leeward ray, hypersonic stream, conical generator, windward ray, aerothermodynamic environment, surface catalycity, aeroassisted orbit transfer vehicles, intersecting shock waves, freestream properties, effective nose radius, conceptual design codes, freestream static temperature, impinging shock wave, misaligned tiles, stagnation point downstream, hypersonic environment, shock wave intersects, stagnation pressure downstream, wetted distance, number independence principle, preflight predictions, bow shock wave, blunt vehicle, hypersonic flow past, noncatalytic surface
Key Phrases - Capitalized Phrases (CAPs):
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Space Shuttle Orbiter, Apollo Command Module, New York, Lessons Learned, Defining the Hypersonic Environment, Hypersonic Shock Tunnel, Langley Research Center, Shuttle Performance, Using Fig, Arnold Engineering Development Center, John Wiley, Academic Press, Ames Research Center, Journal of the Aeronautical Sciences, Journal of the Aerospace Sciences, Aeroassist Flight Experiment, Aerodynamics of Hypersonic Lifting Vehicles, Air Force Flight Dynamics Laboratory, Combining Eqs, Defining the Aerothermodynamic Methodology, Project Fire, Ames Research Staff, Englewood Cliffs, Ibm Fig, Jet Propulsion
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