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.↗
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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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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.↗
Nonmetallic-material selection criteria, test requirements, test techniques and data, and configuration control as applied to manned spacecraft
Manned spacecraft nonmetallic construction materials selection criteria, testing and configuration control, considering flammability hazard
Bland, W. M., Jr.↗
Development, fabrication, testing, and delivery of advanced filamentary composite nondestructive test standards Final report
Development and fabrication of filament composite nondestructive test standards
Lewis, W. H.↗
NERVA irradiation program, GTR test 21. Volume 4 - Effect of radiation on structural materials tested at cryogenic and elevated temperatures
Effect of radiation on structural materials for NERVA engine tested at cryogenic and elevated temperatures - Vol. 4
King, N. D.↗
Static tests of a 0.7 scale augmentor wing flap for the modified C-8A airplane - Test results and analysis
Static tests of augmentor-wing flap system for modified C-8A jet STOL research airplane using 0.7 scale model
Harkonen, D. L.↗
Unified test equipment: A concept for the shuttle ground test system
Development of unified test equipment concept for space shuttle ground support system
Dalke, E. A.↗
Space Shuttle: AEDC Von Karman Tunnel C, Test VT0055 Samso-gd/convair T-18 Hypersonic Static Stability and Control Effectiveness Investigation. Wind Tunnel Test Results
Hypervelocity wind tunnel static stability and control tests of variable geometry configuration of space shuttle
Gallaher, W. H.↗
Fabrication, spin testing and magnetic testing of a welded rotor in a 36000 RPM Lundell alternator
Inconel-steel, puddle-welded rotor spin and magnetic testing for use in 36,000 rpm Lundell alternator
Lumannick, S.↗
Evaluation of SNAP-8 alternator P/N 094069, S/N 481490 after 23130 hours of endurance testing in the Electrical Component Test Facility (ECTF)
Electric-equipment and drive adapter endurance tests for SNAP 8
Foley, R. S.↗
Status of life testing, stress testing, and failure analysis and corrective action
Service life/stress testing, failure analysis and corrective action from technical and cost positions
Bland, W. M., Jr.↗
Definition study for an extended manned test of a regenerative life support system, preliminary test plan
A preliminary plan and procedure are presented for conducting an extended manned test program for a regenerative life support system. Emphasis will be placed on elements associated with long-term system operation and long-term uninterrupted crew confinement.
Source record↗
Orifice In-flow Efficiency Tests. Volume 1: Test Results. Volume 2: Application to Shuttle Venting During Entry
An investigation was made of the capability for computing internal pressures throughout flight for compartments located within space shuttle vehicles. A test program was conducted at a 6 x 6 foot supersonic wind tunnel to determine orifice efficiencies for the flow of air into a compartment from a flowing external stream. Measurements were made over a Mach number range of 0.7 to 1.9 for varying orifice geometry, vent orientation, vent plate thickness, flat plate boundary layer thickness, and pressure ratio across the vent plate. A computer program developed for outflow venting was modified for use in computing compartment pressures for inflow conditions. Results from both the outflow and inflow computer programs are included. A user's manual and program listing of the inflow venting program are also included.
Haukohl, J.↗
Systematic two-dimensional cascade tests. Volume 4: Cascade test data
The data pertaining to the performance characteristics of hydrofoils are presented. The hydrofoils are: (1) double circular arc, (2) multiple circular arc, and (3) slotted doubled circular arc. The experimental data are organized into a systematic presentation format and provided with scale factors and reference values for interpretation. The data include local pressure distributions upstream and downstream of the cascade test section, continuous records from flow angle and total pressure surveys, hydrofoil local pressure distributions, and cavitation data.
Murrin, T. A.↗