The performance of two critical technology components required for a continuously rotatable heat pipe: (1) a low-leakage rotatable coupling for the heat pipe pressure vessel, and (2) a rotatable internal wick, is reported. Performance and leakage requirements were established based on 12 months operation of a cryogenic rotatable heat pipe on a satellite in earth orbit
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
A program was conducted to evaluate and characterize the carbon dioxide-methane (CO2-CH4) decomposit...
The design of the high resolution imager (HRI) on HEAO 2 was modified for use in the instrument comp...
Restructuring research objectives from a technical readiness demonstration program to an investigati...
A flight experiment designed to demonstrate current cryogenic heat pipe technology was defined and e...
The test facility and initial test program developed to experimentally measure the fluid forces indu...
Test program for determining visual reference requirements for pilot control of gliding parachutes u...
An experiment was completed to demonstrate that low ammonia concentrations in the product nitrogen s...
Pressure and heat transfer tests were conducted simulating flight conditions which the space shuttle...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
Data sheets are presented for 11 internal payloads, 30 externally mounted payloads, and 46 free flye...
Various concepts for the design of the nonelectrochemical absorber were defined and evaluated. A pre...
The fabrication of a one-person Electrochemical Depolarized Carbon Dioxide Concentrator subsystem in...
Nozzle material performance data were obtained, and the feasibility was determined of using new mate...
Different magnetic alloys best suited for high-frequency and high-efficiency applications were compa...
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
A program was conducted to evaluate and characterize the carbon dioxide-methane (CO2-CH4) decomposit...
The design of the high resolution imager (HRI) on HEAO 2 was modified for use in the instrument comp...
Restructuring research objectives from a technical readiness demonstration program to an investigati...
A flight experiment designed to demonstrate current cryogenic heat pipe technology was defined and e...
The test facility and initial test program developed to experimentally measure the fluid forces indu...
Test program for determining visual reference requirements for pilot control of gliding parachutes u...
An experiment was completed to demonstrate that low ammonia concentrations in the product nitrogen s...
Pressure and heat transfer tests were conducted simulating flight conditions which the space shuttle...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
Data sheets are presented for 11 internal payloads, 30 externally mounted payloads, and 46 free flye...
Various concepts for the design of the nonelectrochemical absorber were defined and evaluated. A pre...
The fabrication of a one-person Electrochemical Depolarized Carbon Dioxide Concentrator subsystem in...
Nozzle material performance data were obtained, and the feasibility was determined of using new mate...
Different magnetic alloys best suited for high-frequency and high-efficiency applications were compa...
The materials experiment carrier (MEC) is an optimized carrier for near term and advanced materials ...
A program was conducted to evaluate and characterize the carbon dioxide-methane (CO2-CH4) decomposit...
The design of the high resolution imager (HRI) on HEAO 2 was modified for use in the instrument comp...