Experimental design and performance data on carbon dioxide and oxygen control for portable life support system using lithium peroxid
Thermodynamic analysis of Apollo 13 oxygen tank to describe stratification phenomenon preceding tank...
Technical and management studies defining Apollo applications program payload integration task
Although filter inductor designers have routinely tended to specify molypermalloy powder cores for u...
Plant construction costs and manufacturing costs were estimated for the production of solar-grade si...
An innovative creep/fatigue test was run to simulate the temperature, mechanical load, and sodium co...
Two zinc depolarized electrochemical carbon dioxide concentrator concepts were analytically and expe...
The results are presented of an investigation to determine the capability of a monopropellant hydraz...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Prototype space flight experiment package for study of circadian periodicity in pocket mic
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
Promethium isotope heated ammonia microthrustor using heat shield package to maintain temperatur
An experimental investigation was performed to study aircraft fuels at low temperatures near the fre...
Physiological, psychological, and microbiological aspects of 34 days confinement, including 20 days ...
A test bed was fabricated to demonstrate hydrogen/oxygen propulsion technology readiness for the int...
These flights were designed to measure the vertical concentration profile of trace stratospheric spe...
Thermodynamic analysis of Apollo 13 oxygen tank to describe stratification phenomenon preceding tank...
Technical and management studies defining Apollo applications program payload integration task
Although filter inductor designers have routinely tended to specify molypermalloy powder cores for u...
Plant construction costs and manufacturing costs were estimated for the production of solar-grade si...
An innovative creep/fatigue test was run to simulate the temperature, mechanical load, and sodium co...
Two zinc depolarized electrochemical carbon dioxide concentrator concepts were analytically and expe...
The results are presented of an investigation to determine the capability of a monopropellant hydraz...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Prototype space flight experiment package for study of circadian periodicity in pocket mic
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence tha...
Promethium isotope heated ammonia microthrustor using heat shield package to maintain temperatur
An experimental investigation was performed to study aircraft fuels at low temperatures near the fre...
Physiological, psychological, and microbiological aspects of 34 days confinement, including 20 days ...
A test bed was fabricated to demonstrate hydrogen/oxygen propulsion technology readiness for the int...
These flights were designed to measure the vertical concentration profile of trace stratospheric spe...
Thermodynamic analysis of Apollo 13 oxygen tank to describe stratification phenomenon preceding tank...
Technical and management studies defining Apollo applications program payload integration task
Although filter inductor designers have routinely tended to specify molypermalloy powder cores for u...