Water recovery study- electrolytic purification of urine contractor report, jul. 7 - oct. 10, 1964
Design parameter study for urine electrolysis module
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Design parameter study for urine electrolysis module
Researches in aerospace medicine dealing with physiological responses to bed rest, drugs, heat stress, proton irradiation, and water immersion
Procedures for maintenance of space center base utilities
Base support services manual of maintenance procedures and responsibilities
Operation and maintenance manual for Kennedy Space Center roads and grounds service
Manufacturing verification tests for quality assurance and control data management on Voyager spacecraft
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Noise reduction of Boeing 707 during landing approach by modifying turbofan nacelle with polyimide fiber glass acoustic sandwich materials
Cost analysis of turbofan nacelle modifications to minimize fan-compressor noise radiation
Static tests to determine effects of throat inlet concepts on forward-radiated fan noise of 707-320B/C airplanes
Subjective evaluation tests of ground observers on relative noise from acoustically treated engine nacelles of Boeing 707 aircraft
Annotated bibliography of plasma physics research papers including plasma propulsion, plasma radiation, and plasma resonance - conference
Annotated bibliography of research papers presented at plasma physics conference
Annotated bibliography of plasma physics research papers including plasma spectroscopy, crossed field plasma accelerators and electric forces on satellites, and collisionless plasma - conference
Environmental control and life support subsystem for space shuttle orbiter
The initial flight test phase of the modified C-8A airplane was conducted. The primary objective of the testing was to establish the basic airworthiness of the research vehicle. This included verification of the structural design and evaluation of the aircraft's systems. Only a minimum amount of performance testing was scheduled; this has been used to provide a preliminary indication of the airplane's performance and flight characteristics for future flight planning. The testing included flutter and loads investigations up to the maximum design speed. The operational characteristics of all systems were assessed including hydraulics, environmental control system, air ducts, the vectoring conical nozzles, and the stability augmentation system (SAS). Approaches to stall were made at three primary flap settings: up, 30 deg and 65 deg, but full stalls were not scheduled. Minimum control speeds and maneuver margins were checked. All takeoffs and landings were conventional, and STOL performance was not scheduled during this phase of the evaluation.
The EVA Contactor four door sedan, an electric passenger vehicle, was tested to characterize the state-of-the-art of electric vehicles. It is a four passenger sedan that was converted to an electric vehicle. It is powered by 16 series connected 6 volt electric vehicle batteries through a four step contactor controller actuated by a foot accelerator pedal. The controller changes the voltage applied to the separately excited DC motor. The braking system is a vacuum assisted hydraulic braking system. Regenerative braking was also provided.
Chemical/hydrogen energy system contracts were reviewed. The review served as an effective means to (1) give all contracts an insight into the background and objectives of thirty-nine hydrogen-related tasks, (2) show the status of the studies or technical effort, (3) relate any problems that had impeded the progress, and (4) state projected solutions for resolving the identified problems.