Saturn S-4B-507 narrative end item report
Manufacturing and checkout test data summary for Saturn S-4B flight stage
Reitzell, W. M.↗
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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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Saturn S-4B-510 narrative end item report
Saturn S-4B-510 flight stage manufacture and checkout procedures
Reitzell, W. M.↗
Huntington Beach narrative end item report - Saturn S-4B-508
Checkout of Saturn S-4B stage
Reitzell, W. M.↗
Saturn S-4B-210 - Narrative end item report
Manufacturing and stage checkout summaries for Saturn S-4B-210 stage
Reitzell, W. M.↗
ACE-SC computer programming system
Acceptance checkout equipment - spacecraft computer programming systems
Murphy, W. T.↗
Sacramento Narrative End Item Report - Saturn S-4B-508
Checkout testing of Saturn S-4B-508 flight stage
Reitzell, W. M.↗
Sacramento narrative end item report - Saturn S-4B-506N
Checkout test data on Saturn S-4B-506N flight stage
Reitzell, W. M.↗
Calibration, simulation, and testing of large orbiting stellar observatories
Calibration, simulation, and checkout testing of large orbiting stellar observatories
Diggins, J. L.↗
Quality assurance requirements manual for planetary spacecraft to be sterilized by heating
Information and guidelines on quality assurance requirements for production, assembly, and checkout of spacecraft to be sterilized by heating
Source record↗
Apollo 8 Mission Report
Postflight analysis of Apollo 8 mission. Apollo 8 was the second manned flight in the program and the first manned lunar orbit mission. The crew were Frank Borman, Commander; James A. Lovell, Command Module Pilot; and William A. Anders, Lunar Module Pilot. The Apollo 8 space vehicle was launched on time from Kennedy Space Center, Florida, at 7:51:00 AM, EST, on December 21, 1968. Following a nominal boost phase, the spacecraft and S-IVB combination was inserted - into a parking orbit of 98 by 103 nautical miles. After a post-insertion checkout of spacecraft systems, the 319-second translunar injection maneuver was initiated at 2:50:37 by reignition of the S-IVB engine.
Source record↗
Automatic Malfunction Analysis
Automatic Malfunction Analysis /AMA/ digital computer software system supporting checkout and testing, defining normal system status by computer simulation
Jaegly, R. L.↗
A new standard for information processing systems for manned space flight
Spaceborne information processing for manned missions, describing layered system with fault tolerance and onboard checkout
Hopkins, A. L., Jr.↗
FORTRAN 4 digital program changer
Computer program modifies other source language programs as aid to debugging, checkout and final documentation to eliminate manual performance of rearranging and incrementing statement numbers, identifying and sequencing cards and inserting and/or removing end-of-batch symbols.
Madden, M. F.↗
Acceptance test, data reduction procedure and calculation definitions used for sealed, absolute, gage and differential strain gage pressure transducers
Checkout and data reduction procedures for acceptance test of sealed, absolute, gage, and differential strain gage pressure transducers
Source record↗
Development of onboard equipment for space shuttle propulsion systems
Development of onboard checkout equipment for space shuttle propulsion systems
Source record↗
Fault isolation computer methods
Computer methods for fault isolation in systems checkout
Garzia, R. F.↗
Space shuttle operations, maintenance and technology integration
Space shuttle operations, maintenance, and integration of ground support system, logistics, checkout, and recovery
Gay, C. C., Jr.↗
Logic devices for the readiness assessment of mechanical components
Logic devices for readiness assessment and checkout of airborne and ground equipment mechanical components
Hartung, D. J.↗