Environmental acceptance test specification for the flight model uk-2/s-52 spacecraft
Test specifications for flight model UK-2/S-52 SPACECRAFT to demonstrate performance under various environments
ENVIRONMENTAL TESTING↗
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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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Evaluation program for secondary spacecraft cells. acceptance test of gulton industries, inc. 5.0 ampere-hour nimbus cells
Performance test evaluation of nickel-cadmium Nimbus secondary spacecraft cells
SPACECRAFT COMPONENT↗
Asymptotic cones of acceptance of cosmic ray neutron monitors in a geomagnetic field dis- torted by the solar wind
Cosmic ray neutron monitors in geomagnetic field distorted by solar wind
NEUTRON DETECTOR↗
Evaluation program for secondary spacecraft cells. acceptance test of sonotone corpora- tion 3.0 ampere-hour triple seal nickel cadmium cells
Phenolphthalein leakage, capacity, cell short, immersion seal, overcharge, and internal resistance tests on nickel-cadmium battery
RESISTANCE↗
Nutritional acceptability of a dehydrated diet.
Nutritional evaluation of precooked dehydrated diet for humans, discussing gastrointestinal stress
NUTRITIONAL REQUIREMENT↗
Plug-in connector socket accepts coaxial cable end
Connector which includes a spring-loaded contact to receive a protruding center conductor and an internal collet to clamp against a collar attached to a woven outer conductor, is used as a receptacle for the end of a coaxial cable. This plug-in connector socket is used successfully with remote manipulators.
Mitchell, D.↗
Quality control criteria for acceptance testing of cross-wire welds
Visual inspection criteria assure the metallurgical integrity of spot welds joining nickel leads and nickel ribbon in a 90 degree cross-wire configuration.
Bryant, R. D.↗
Evaluation program for secondary spacecraft cells. Acceptance test of Gulton Industries, Inc. 1.25 ampere-hour nickel cadmium cells with high overcharge capabilities
Performance of sealed nickel-cadmium spacecraft batteries with high overcharge capability
SPACECRAFT↗
Evaluation program for secondary spacecraft cells. Acceptance test of Sonotone Corporation 3.5 ampere-hour sealed nickel-cadmium cells
Leak, capacity, overcharge, and internal resistance tests of ceramic sealed nickel cadmium secondary spacecraft cells
STORAGE BATTERY↗
Evaluation program for secondary spacecraft cells. Acceptance test of C and D batteries, 5.0 ampere-hour sealed-calcium cells
Leak, capacity, overcharge, and internal resistance tests of sealed lead-calcium secondary spacecraft cells
SPACECRAFT POWER SUPPLY↗
The flow induction process of compressors designed to accept supersonic inflow velocity.
Supersonic compressor flow induction process as affected by Mach number, cone angle, rotational speed and blade angle
MACH NUMBER↗
Evaluation program for secondary spacecraft cells - Acceptance test of Gulton Industries Incorporated 12 and 20 ampere-hour adhydrode cells
Performance evaluation tests on secondary spacecraft cells
SPACECRAFT↗
Joint acceptance for cylinders
Theoretical analysis of response of thin cylindrical shell to random vibratory loading
VIBRATORY LOADING↗
Failure rates for accelerated acceptance testing of silicon transistors
Extrapolation tables for the control of silicon transistor product reliability have been compiled. The tables are based on a version of the Arrhenius statistical relation and are intended to be used for low- and medium-power silicon transistors.
Toye, C. R.↗
Rapid pumpdown system for NASA's Sunspot 1 Facility Final report and acceptance test results
Explore the source record for details and available documents.
Gaffney, C.↗
ACE-S/C equipment description - Acceptance checkout equipment-spacecraft
Explore the source record for details and available documents.
Source record↗
Saturn S-4B-505N stage acceptance firing report. Special cold helium test, addendum
Flight simulation data of Saturn S-4B cold helium tests
Source record↗
Establishment of design criteria for acceptable failure modes and fail safe considerations for the space shuttle structural system
The application of general design approaches for preventing failures due to repeated load cycles is briefly discussed. Program objective, mission requirements, and structural design criteria are summarized. Discrete structural elements and associated sections were selected for detailed strength, fatigue, and fracture mechanics investigations.
Westrup, R. W.↗