The Concentration of Depleted Uranium (DU) and Beryllium (BE) in Soil and Air on Illeginni Island at Kwajalein Atoll after an AHW Flight Test
Abstract not provided.
42 ENGINEERING↗
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Results for “Flight Test”
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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AERODYNAMIC OBSERVATIONS FROM FLIGHT TESTS OF TWO VTOL AIRCRAFT
Effect of ground proximity, wing-stall phenomena, pitching moments, and power requirements on vtol aircraft
GROUND EFFECT↗
AUTOMATIC ANALYSIS OF LAUNCH VEHICLE FLIGHT TEST
Evaluation and checkout of saturn class launch vehicles using ibm 7090 computer
COMPUTER PROGRAM↗
SYSTEM CHECKOUT AND FLIGHT TESTING OF UNMANNED LUNAR AND PLANETARY SPACECRAFT
Test equipment, facilities and types of tests involved in system checkout of the ranger and mariner spacecrafts
SYSTEMS ANALYSIS↗
Current status of the solid-propellant flight- test vehicle
Solid propellant rocket vehicles
SOLID PROPELLANT ROCKET ENGINE↗
Free-flight tests of a blunt-nosed flare- stabilized body at speeds to 8.2 km/sec.
Static and dynamic stability and drag of blunt- nosed flare-stabilized bodies at velocities up to 8.2 kilometers per second
FLARED BODY↗
Application of the time vector method to the analysis of flight test lateral oscillation data
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Larrabee, E. E.↗
An evaluation of free-flight test data for aerodynamic heating from laminar, turbulent, and transitional boundary layers. Part II - The X-17 reentry body
Blunt body reentry vehicle aerodynamic heating determination
REENTRY VEHICLE↗
Minimum Drag of Four Versions of a Swept-wing Fighter Airplane Obtained from Flight Tests of Rocket-boosted Models at Mach Numbers from 0.81 to 1.71
Swept wing fighter aircraft drag coefficient reduction by configuration redesign
AIRCRAFT CONFIGURATION↗
Free-flight tests of a blunt-nosed flare- stabilized body at speeds to 8.2 km/sec.
Static and dynamic stability and drag of blunt- nosed flare-stabilized bodies at velocities up to 8.2 km per second
STATIC STABILITY↗
Study to determine the flight test objectives for ion propulsion systems Preliminary report, 1 Mar. - 15 May 1961
Electrostatic propulsion requirements and ion engine testing methods
ELECTROSTATIC PROPULSION↗
TEMS radar error model regression analysis results from the Saturn AS-201, AS-202, and SA-203 flight tests
Tracking system error model regression analysis results from Apollo-Saturn tests
REGRESSION ANALYSIS↗
Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods
Afterbody heating by Mercury spacecraft during reentry determined from skin temperatures
MERCURY CAPSULE↗
Pre-flight testing of the ATS-1 thermal coatings experiment.
Preflight testing of ATS-1 Thermal Coatings Experiment /TCE/, discussing cup designs, sensor and cup calibrations, etc
PROTECTIVE COATING↗
Study to determine the flight test objectives for ion propulsion systems monthly progress report, jul. 1961
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Kalensher, B. E.↗
Calculation of the dynamic longitudinal stability of a tilt-wing V/STOL aircraft and correlation with model flight tests
Aerodynamic factors, and effects on dynamic longitudinal stability characteristics of tilt wing V/STOL aircraft
Chambers, J. R.↗
Results from SERT I ion rocket flight test.
SERT 1 /Space Electric Rocket Test/ spacecraft /launched July 20, 1964/ test results
Cybulski, R. J.↗
Large-scale decelerator flight tests simulating a Mars environment.
Large scale parachute tests of aerodynamic decelerator systems at 132,000 ft simulating conditions of Mars atmosphere at 15,000 ft
Darnell, W. L.↗