Ranger TV subsystem flight evaluation report for flight model III-1 /RA-6/ and design review report
Flight evaluation on Model III /RA-6/ of Ranger television subsystem - failure analysis
FAILURE↗
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Preliminary launch vehicle flight evaluation report NASA Applications Technological Satellite /ATS/ program flight no. 1, NASA ATLAS - Agena no. 19 /launched December 6, 1966/
Applications Technology Satellite-1 Atlas Agena launch vehicle flight performance evaluation
APPLICATIONS TECHNOLOGY SATELLITE /ATS/↗
Flight vibration data of Astrobee 1500, NASA flight 16.02 Final report
Flight vibration data of Astrobee 1500 rocket vehicle
Munson, A. N.↗
Measurement of aerodynamic derivatives in wind tunnels and in flight. Part 1 - Research in wind tunnels. Part 2 - Determination in flight of the aerodynamic coefficients of an aircraft by the study of its frequency response
Measuring aerodynamic derivatives in wind tunnels and in-flight and determining aerodynamic coefficients of aircraft by frequency response
Mathe, P.↗
Instrumentation and flight report on Astrobee 1500 flight 16.02 GT
Astrobee 1500 flight test
Tackett, C. D.↗
Space Flight Handbooks. Volume 3, Planetary Flight Handbook: Mars Stopover Missions Using Venus Swingbys - Part 6
This volume of the NASA Planetary Flight Handbook contains trajectory data to aid the mission analyst in the planning of stopover missions to Mars that employ the Venus swingby mode. Compared to other mission modes, the Venus swingbys yield substantial reductions in propulsive velocity and Earth entry speed requirements when employed as part of a round trip stopover mission. Conversely, the swingbys are at best, of marginal utility for one-way missions. Consequently, this Handbook has been tailored expressly for use in the planning of round trip missions. The relevant charts, graphs, and tabular data are presented for the totality of such missions, i.e., in terms of total round trip mission duration and stopover time at Mars. Recognizing, however, that within the context of round trip missions the single-leg data can be of importance in certain phases of the mission analyses, all such data has been preserved on a master magnetic tape. Copies of this tape will be made available to interested organizations.
Source record↗
Study of flight management requirements during SST low visibility approach and landing operations. Volume 2 - Delineation of potential problems in supporting the performance of flight management tasks
Potential flight management problems during low visibility landing of supersonic transports
Gartner, W. B.↗
Study of flight management requirements during SST low visibility approach and landing operations. Volume 3 - Recommendations for a simulation research study of selected flight management support problems
Simulation objectives and requirements for flight management problems during low visibility approach and landing of supersonic transports
Gartner, W. B.↗
Space-flight mission design for flight and crew safety.
Manned space flight safety through mission trajectory design, considering hardware, software and operational constraints
Allen, C. C.↗
NASA Science and Technology Advisory Committee for Manned Space Flight. Winter Study on Uses of Manned Space Flight, 1975-1985. Volume 1 - Proceedings
Manned space flight capabilities for lunar and planetary explorations and earth orbiting stations
Source record↗
Space flight handbooks, volume 3. Planetary flight handbook, part 7 - Direct trajectories to Jupiter, Saturn, Uranus, and Neptune. General discussion, contour charts and related graphical information
Planetary flight handbook - direct trajectories to Jupiter, Saturn, Uranus, and Neptune
Source record↗
Instrumentation and flight performance of HCO high resolution wavelength spectrometer - NASA Aerobee flight 4.185 US
Flight performance of high resolution spectrometer in Aerobee rocket vehicle
Parkinson, W. H.↗
US manned space flight - The manned flight program, the astronauts
Mercury, Gemini, and Apollo manned flight operational and personnel data
Source record↗
ERC V/STOL program flight test plan. H-19 flight program phases 1A and 1B, Wallops Station, Virginia
Flight test program to obtain data on aided inertial system for terminal guidance and navigation of helicopter in designing V/STOL avionics system
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Space Flight Handbooks, Volume 3 - Planetary Flight Handbook. Part 8 - Jupiter Swingby Missions to Saturn, Uranus, Neptune, and Pluto. Supplement - Tabular Trajectory Data
The trajectory data are presented chronologically and are organized by holding the arrival date constant while varying the Earth departure date in increments of 10 days. Upon completion of the specified range of Earth departure dates, the arrival date is incremented and the range of departure dates is repeated. The range of departure and arrival dates and the corresponding increments are given in Table 5-1 for each launch opportunity. It should be noted that the interval in arrival date is increased in the long flight time region where the variation of the trajectory parameters is relatively small. The criteria used for the selection of these dates are, in general: (i) the minimum Earth departure hyperbolic excess speed (across the Earth departure window) shall not exceed 0.65 EMOS and (2) the periapsis radius at Jupiter shall not be less than 0.95 planet radii.
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A theoretical and flight test study of pressure fluctuations under a turbulent boundary layer. Part 2: Flight test study
The study of pressure fluctuations under a turbulent boundary layer was undertaken with the objective of extending previous work to lower frequencies. Wind tunnel and flight test measurements are invalid at low frequencies because of extraneous acoustic noises and free stream turbulence. A glider was instrumented and used as a test bed to carry microphones into a smooth flow free of acoustic noise. Hodgson had previously measured the spectrum of boundary layer noise on a glider wing. These tests showed a drop off at low frequencies that could not be reproduced in any other facility. The measurements were made on the forward fuselage of a glider where the boundary layer could develop naturally and have some length in a zero pressure gradient before the measurements were made. Two different sets of measurements were made.
Panton, R. L.↗
A new flight test data system for NASA aeronautical flight research
The airborne integrated flight test data system (AIFTDS) is described. This system integrates an airborne digital computer with a high-bit-rate pulse code modulation system. Its design was influenced by in-house technical experience with similar modules and by the multiproject environment in which it was expected to operate. The present work describes events leading to the development of the system, reviews factors that influenced the objectives for the system and the resulting design, and describes the elements themselves. Block diagrams supplement the text.
Sanderson, K. C.↗
A study of Mariner 10 flight experiences and some flight piece part failure rate computations
The problems and failures encountered in Mariner flight are discussed and the data available through a quantitative accounting of all electronic piece parts on the spacecraft are summarized. It also shows computed failure rates for electronic piece parts. It is intended that these computed data be used in the continued updating of the failure rate base used for trade-off studies and predictions for future JPL space missions.
Paul, F. A.↗