A method for making large-scale decelerator tests in a simulated 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.↗
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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.↗
Summary of the development status of attached inflatable decelerators.
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Bohon, H. L.↗
Status of research on parawing lifting decelerators.
Flexible parawing lifting decelerator research data from wind tunnel and flight tests, noting manned space vehicle recovery and aircraft escape systems
Gainer, T. G.↗
Aerodynamic deceleration systems for space missions.
Aerodynamic deceleration systems for space missions, considering deployment of subsonic parachute and inflatable configuration following atmospheric entry
Gillis, C. L.↗
Performance of a towed, 48-inch-diameter /121.92-cm/ ballute decelerator tested in free flight at Mach numbers from 4.2 to 0.4
Inflation, drag, and stability characteristics of towed inflatable ballute decelerator at free flight
Usry, J. W.↗
Dynamics of towed decelerators
Two body mathematical model for flexible tow line- decelerator dynamical system
Campbell, J. F.↗
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.↗
Static longitudinal aerodynamic characteristics of some supersonic decelerator models at Mach numbers of 2.30 and 4.63
Aerodynamic characteristics of blunted cones, tension shell, and attached inflatable decelerator models
Davenport, E. E.↗
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.↗
Deceleration-control system for aerobraking and skipout to orbit at Mars.
Deceleration control system for aerobraking and skipout to orbit at Mars
Schy, A. A.↗
Evaluation of entry and terminal deceleration systems for unmanned Martian landers.
Entry and terminal deceleration systems for unmanned Martian landers, discussing parachute landing and lifting entry vehicles
Harrison, E. F.↗
Development status of attached inflatable decelerators.
Structural and aerodynamic developments in attached inflatable decelerators for deployment of payload at supersonic speeds
Bohon, H. L.↗
Deceleration control system for aerobraking and skipout to orbit at Mars.
Deceleration control system for aerobraking and skipout to orbit at Mars
Schy, A. A.↗
Deployable aerodynamic decelerators for space missions.
Aerodynamic deceleration systems for space missions, considering deployment of subsonic parachute and inflatable configuration following atmospheric entry
Gillis, C. L.↗
Limits on the cosmological deceleration parameter.
Deceleration parameter lower and upper limits for zero pressure big bang cosmological Friedmann models imposed by density parameter, Hubble constant and universe age
Rindler, W.↗
Status of research on parawing lifting decelerators.
Flexible parawing lifting decelerator research data from wind tunnel and flight tests, noting manned space vehicle recovery and aircraft escape systems
Gainer, T. G.↗
A structural merit function for aerodynamic decelerators
Structural merit function for aerodynamic decelerators
Anderson, M. S.↗