Research-Airplane-Committee Report on Conference on the Progress of the X-15 Project : A Compilation of the Papers PresentedThis document is a compilation of papers presented at the Conference on the Progress of the X-15 project held at the IAS Building, Los Angeles, California, July 28-30, 1958. The conference was held by the Research Airplane Committee of the U. S. Air Force, the U. S. Navy, and the National Advisory Committee for Aeronautics to report on the technical status of this airplane.
IDRelationTitle19930092391WorkPilot protection for the X-15 aircraft19930092394WorkWind-tunnel investigation of the heat transfer to the X-15 airplane19930092388WorkCentrifugal simulation of the X-1519930092404WorkX-15 auxiliary power units and reaction controls19930092406WorkX-15 conditioning and pressurization system19930092395WorkEffects of aerodynamic heating on X-15 temperatures19930092389WorkDevelopment of X-15 escape system19930092405WorkLand-gear design and development testing19930092385WorkLow-speed stability and control and spinning characteristics of dynamic models of the X-15 airplane19930092382WorkHigh-speed static stability characteristics of the X-15 airplane19930092392WorkStatus of high-range and flow-direction sensor19930092384WorkThe measured and estimated rotary stability derivatives of the X-15 airplane19930092383WorkEffects of rocket jet on stability and control at high Mach numbers19930092393WorkAll-attitude flight-data system for the X-15 research airplane19930092381WorkX-15 research airplane development status19930092387WorkX-15 flight simulation studies19930092403WorkX-15 hydraulic-system development19930092407WorkX-15 research objectives19930092390WorkAeromedical support of the X-15 program19930092381WorkX-15 research airplane development status19930092382WorkHigh-speed static stability characteristics of the X-15 airplane19930092383WorkEffects of rocket jet on stability and control at high Mach numbers19930092384WorkThe measured and estimated rotary stability derivatives of the X-15 airplane19930092385WorkLow-speed stability and control and spinning characteristics of dynamic models of the X-15 airplane19930092387WorkX-15 flight simulation studies19930092388WorkCentrifugal simulation of the X-1519930092389WorkDevelopment of X-15 escape system19930092390WorkAeromedical support of the X-15 program19930092391WorkPilot protection for the X-15 aircraft19930092392WorkStatus of high-range and flow-direction sensor19930092393WorkAll-attitude flight-data system for the X-15 research airplane19930092394WorkWind-tunnel investigation of the heat transfer to the X-15 airplane19930092395WorkEffects of aerodynamic heating on X-15 temperatures19930092403WorkX-15 hydraulic-system development19930092404WorkX-15 auxiliary power units and reaction controls19930092405WorkLand-gear design and development testing19930092406WorkX-15 conditioning and pressurization system19930092407WorkX-15 research objectives