Space environment simulator test program. Volume 2 - Unmanned thermal performance evaluation of a Gemini extravehicular space suit Test report, May 1965
Temperature data plots of Gemini Bravo series space suit tests
Copeland, R. J.↗
SEARCH · Engineering Papers
Results for “Testing.”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Two-stage potassium test turbine. Volume 3 - Test facilities
Design, and performance of facility for Rankine cycle testing of two stage potassium vapor turbine
Eckard, S. E.↗
Apollo Applications Program /AAP/ payload integration - General test plan, combined mission, flights AAP 1/2/3/4. Volume 1 - Test program summary
Test program summary for Apollo Applications Program combined mission payload integration
Source record↗
Pressure test analysis of 200-inch multicell test tank
Pressure test analysis for large multiple cell tank with sectioned skin
Burnette, M. F.↗
Study of space battery accelerated testing techniques. Phase 1 report. Survey of testing methods applicable to space battery evaluation
Testing methods applicable to space battery evaluation - literature survey
Brooman, E. W.↗
Sixty-day manned test of a regenerative life support system with oxygen and water recovery. Part 1 - Engineering test results
Engineering results of 60-day manned test of regenerative life support system with oxygen and water recovery in spacecraft cabin simulator
Source record↗
Test plan for NAVSTAR navigation system. Volume 1 - Test plan description
Performance test plan of radio navigation system employing satellite
Source record↗
Test plan for NAVSTAR navigation system. Volume 2 - ERS test satellite design
Environmental research satellite test design with transponder for range measurements at ground station
Source record↗
Nickel-cadmium battery test project - Relationship between operation, life and failure mechanism. Volume 2 - Battery test results
Factors influencing cyclic life of nickel cadmium batteries - tabulated test results
Halpert, G.↗
Ludwieg tube pilot test and high Reynolds number test equipment
Test facility and equipment to determine very high Reynolds number effects associated with large boost vehicles
Davis, J. W.↗
Spacecraft Attitude Control System, Prototype and Test Final Analysis and Test Report
Performance tests of prototype liquid ammonia spacecraft attitude control systems
Cromwell, R.↗
Solder study conducted on Apollo telescope mount gyro processor /group 1 and 2 tests/ Final test report
Thermal cycling machines and accelerated test techniques to improve solder joints for Apollo Telescope Mount
Diel, D. F.↗
Test report on fatigue-testing of nickel-200 panels
Nickel-200 fatigue testing for thermal fatigue data on regeneratively cooled hypersonic research engine structures
Biastre, F. A.↗
Study of space battery accelerated testing techniques. Phase 2 report - Ideal approaches towards accelerated tests and analysis of data
Ideal approaches to accelerated life tests and data analysis applied to space batteries
Brooman, E. W.↗
Apollo/Surveyor test plan. Plan for postflight test and analysis of parts and materials of Surveyor 3, retrieved from lunar surface by Apollo 12. Volume 1 - Technical plan
Postflight test and analysis of parts and material of Surveyor 3 retieved from lunar surface by Apollo 12
Source record↗
Static testing of the San Marco 2 satellite - Tests of the temperature control system
Static testing of San Marco 2 satellite and its temperature control system
Arduini, C.↗
Dynamic testing of Apollo spacecraft in the flight environment /stroking test/ - Project Apollo
Proposed dynamic flight testing of Apollo spacecraft
Peters, W. H.↗
Determination of processing and test facility requirements for large solid rocket motors. Volume 1 - Task 1 - Facility modification for full-length 260 inch diameter motor processing and test Final report
Facility modification plan for testing 260-inch diameter solid rocket engine
Lambert, W. L.↗