1972 NASA Authorization: Hearings, Ninety-second Congress, First Session, on H.R. 3981 (superseded by H.R. 7109)U.S. Government Printing Office, 1971 |
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aerodynamic aeronautical aircraft noise airplane airport application avionics basic research capability characteristics clear air turbulence combustor components concepts conducted configurations continue CTOL dynamic effects effort electrical electronic evaluation experimental fiscal year 1972 flap flight dynamics Flight Research flight test flow fuel element funding heat shield HECHLER hydrogen hypersonic improved increase investigated JACKSON laboratory landing Langley Research Center laser Mach number materials ment missions NASA NERVA nozzle nuclear rocket OART operating orbit performance pilot planetary planned plug nozzle potential power systems problems propellant propulsion system reactor reduce research and technology research program rotor runway safety shown in Figure SHUTTLE TECHNOLOGY simulator sonic boom space shuttle spacecraft specific impulse speed STOL STOL aircraft structural studies supercritical supercritical wing supersonic techniques technology program temperature thermal thrust thruster tion turbine V/STOL vehicle VTOL wind tunnel wing WYDLER