Results from SERT I ion rocket flight test.
SERT 1 /Space Electric Rocket Test/ spacecraft /launched July 20, 1964/ test results
Cybulski, R. J.↗
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Results for “Flight tests”
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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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.↗
Flight-test results of gamma ray scattering as a technique for air-density measurement
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Reichle, H. G., Jr.↗
Flight-test results from supersonic deployment of an 18-foot-diameter /5.49 meter/ towed ballute decelerator
Supersonic deployment and extraction of inflatable towed ballute decelerator
Eckstrom, C. V.↗
Results of a free-flight test to determine the performance characteristics of a towed, conical decelerator
Drag and stability characteristics of towed, conical decelerator
Usry, J. W.↗
Flight test results of a trailing edge flap designed for direct-lift control
Boundary layer control and trailing edge flaps for direct-lift control
Taylor, C. R., Jr.↗
Flight test of a solid-fuel ramjet with the internal surface of the combustor air cooled
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Bartlett, W. A., Jr.↗
Mercury ground and flight-test program
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Bland, W. M., Jr.↗
Some Effects of Roll Rate on the Longitudinal Stability Characteristics of the Hughes Falcon Missile, ''C'' Configuration, for a Mach Number Range of 1.1 to 1.8 as Determined from Flight Test
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Baber, H. T., Jr.↗
Flight test of a 40 foot nominal diameter disk-gap-band parachute deployed at a Mach number of 3.31 and a dynamic pressure of 10.6 pounds per square foot
Performance test on disk gap band parachute at supersonic speeds
Eckstrom, C. V.↗
Accuracy of determining sensor boresight position during aircraft flight-test
Nonimaging remote sensor data display in spatial registration with ground scene to determine sensor boresight position accuracy
Eppler, W. G.↗
Ground and flight test results of a decelerator towline energy absorber
Parachute decelerator towline energy absorber shock attenuation characteristics, discussing drop test results
Councill, E. L., Jr.↗
Results from SERT 1 ion rocket flight test
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Cybulski, R. J.↗
Fluidic wind sensor research leading to a flight test model Final report
Flow visualization study of flyable fluidic low speed wind sensor
Neradka, V. F.↗
Vertical-Tail Loads and Control-surface Hinge-Moment Measurements on the M2-F2 Lifting Body During Initial Subsonic Flight Tests
Vertical tail loads and control surface hinge moment measurements on M2-F2 lifting body at subsonic speeds
Jenkins, J. M.↗
Aerodynamics of a model of the HL-10 flight- test vehicle at Mach 0.35 to 1.80
Aerodynamic characteristics of HL-10 reentry vehicle model at subsonic and supersonic speeds
Hill, A. S.↗
Ground and flight test results for a decelerator towline energy absorber
Parachute decelerator towline energy absorber shock attenuation characteristics, discussing drop test results
Councill, E. L., Jr.↗
Project RAM flight-test rocket vehicles
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Raper, J. L.↗