POWER SOURCE FOR A ONE KILOWATT ARC ENGINE TEST CAPSULE
Power source for a one kilowatt arc engine test capsule
ARC JET↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.40 TO 1.20 OF THE STATIC AERODYNAMIC AND CONTROL CHARACTERISTICS OF A MODEL OF A NONLIFTING REENTRY CAPSULE IN COMBINATION WITH A ROCKET BOOSTER
Wind tunnel investigation at subsonic & transonic speed of static aerodynamic and control characteristics of capsule-booster model
CONTROL↗
FREE-FLIGHT MEASUREMENTS OF STATIC AND DYNAMIC STABILITY OF MODELS OF THE PROJECT MERCURY RE-ENTRY CAPSULE AT MACH NUMBERS 3 AND 9.5
Static & dynamic stability of mercury reentry capsule scale models at mach 3 & 9.5
REENTRY VEHICLE↗
Investigation of foamed metals for application on space capsules annual report, 29 jun. 1963 - 15 aug. 1964
Foamed metal development for space capsules - brazing, variable density beam, thermal testing, mechanical tests, and machining
SPACE CAPSULE↗
Separation tests of rocket-propelled models of a pilot-escape capsule
Separation of jettisonable-nose pilot-escape capsule investigation by means of rocket-model flight tests
ESCAPE CAPSULE↗
Development of highly reliable capsule type slip ring assemblies final summary report
Design materials and processes for improvement of slip ring capsule assemblies
CAPSULE↗
Transonic Dynamic Stability Characteristics of Several Models of Project Mercury Capsule Configurations
Transonic dynamic stability characteristics of Mercury capsule scale model configurations
TRANSONIC SPEED↗
Human water exchange in space suits and capsules
Human water exchange in space suits and capsules
PHYSIOLOGICAL RESPONSE↗
A compilation of wind-tunnel heat-transfer measurements on the afterbody of the Project Mercury capsule reentry configuration
Compilation of wind-tunnel heat-transfer measurements on afterbody of Mercury capsule reentry configuration
REENTRY BODY↗
Pressure and heat-transfer distribution on the afterbody of a lifting Mercury- type capsule at Mach number 15 in helium
Afterbody pressure and heat transfer distribution, shock wave shapes, and photographs of local flow conditions for Mercury type capsule at Mach number 15 in helium
AFTERBODY↗
Wind-tunnel investigation at Mach numbers from 3.0 to 6.8 of the static aerodynamic characteristics of modified Mercury exit and escape capsule configurations
Static aerodynamic characteristics of modified Mercury exit and escape capsule configurations at Mach numbers 3.0 to 6.8
STATIC STABILITY↗
Effectiveness of Several Control Arrangements on a Mercury-Type Capsule
Trim effectiveness of aerodynamic control flaps on Mercury-type capsule
MERCURY CAPSULE↗
Voyager capsule, preliminary design, phase B. Volume I - Summary Final report
Integrated test plan and implementation plan highlights for Voyager capsule - preliminary design phase B
SYSTEMS DESIGN↗
Voyager capsule, preliminary design, phase B. Volume III - Surface laboratory system. Section I - Surface laboratory Final report
Surface Laboratory preliminary configuration for Voyager mission - space capsule
SPACE CAPSULE↗
Voyager capsule, preliminary design, phase B. Volume III - Surface laboratory system. Section II - Preliminary design for OSE FINAL report
Operational support equipment and mission dependent equipment for preliminary design of surface laboratory portion of Voyager capsule bus system
PLANETARY SURFACE↗
Voyager capsule, preliminary design, phase B. Volume IV - Entry science package. Section I - Entry science package Final report
Entry Science Package preliminary design for Voyager flight capsule
ELECTRONIC PACKAGING↗
Voyager capsule, preliminary design, phase B. Volume IV - Entry science package. Section II - Preliminary design for OSE FINAL report
Operational support equipment preliminary design for entry science package portion of Voyager flight capsule system
GROUND SUPPORT EQUIPMENT↗
Voyager capsule, preliminary design, phase B. Volume IV - Entry science package. Section V - Interfaces Final report
Hardware, software, and service interfaces between capsule bus, entry science package, and Voyager spacecraft
SPACE CAPSULE↗