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8
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Supersonic Inflatable Aerodynamic Decelerators for Use on Future Robotic Missions to Mars
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9
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High Mass Mars Entry, Descent, and Landing Architecture Assessment
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11
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15
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77952830322
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Investigation to Determine the Feasibility of Using Inflatable Balloon Type Drag Devices for Recovery Applications in the Transonic, Supersonic, and Hypersonic Flight Regime Part II: Mach 4 to Mach 10 Feasibility Investigation
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16
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17
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"Aerodynamic Characteristics of Towed Spheres, Conical Rings, and Cones Used as Decelerators at Mach Numbers from 1.57 to 4.65
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An Investigation of the Deployment Characteristics and Drag Effectiveness of the Gemini Personnel Decelerator at Subsonic and Supersonic Speeds, Phase II
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20
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77952831203
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Pressure Measurements on the Rigid Model of a Balloon Decelerator the Wake of a Simulated Missile Payload at Mach Numbers 1.5 to 6.0
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AEDC TDR-64-65, April
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Bell, D.R., "Pressure Measurements on the Rigid Model of a Balloon Decelerator the Wake of a Simulated Missile Payload at Mach Numbers 1.5 to 6.0," ARO Inc. Technical Report, AEDC TDR-64-65, April 1964.
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21
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77952847549
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Longitudinal Stability Characteristics of Several Proposed Planetary Entry Vehicles at Mach 6.73
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April
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22
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77952835178
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Wind Tunnel Investigation of Flexible Aerodynamic Decelerator Characteristics at Mach Numbers 1.5 to 6.0
-
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77952872443
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Exploratory Experimental Aerodynamic Investigation of Tension Shell Shapes at Mach 7
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AFCRL 65-877, December
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Graham Jr., J.J., "Development of Ballute for Retardation of Arcas Rocketsondes," Goodyear Aerospace Corporation Contractor Report, AFCRL 65-877, December 1965.
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26
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48849092443
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Experimental Investigation to Determine Utility of Tension Shell Concept
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27
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77952792508
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Longitudinal Aerodynamic Characteristics of a Tension Shell Entry Configuration at Mach 20
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28
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85002857655
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30
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77952803630
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Transonic Aerodynamic Investigation of Tension Shell and Blunted 100° Conical Shapes for Unmanned Entry Vehicles
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-
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32
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Experimental Flow Field and Heat-Transfer Investigation of Several Tension Shell Configurations at a Mach Number of 8
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Jones, R.A.1
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33
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34
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-
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36
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Deployment Mechanics for an Inflatable Tension-Cone Decelerator
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37
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Static Aerodynamic Characteristics of Blunted Cones in the Mach-Number Range from 2.2 to 9.5
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38
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Investigation of an Attached Inflatable Decelerator System for Drag Augmentation of the Voyager Entry Capsule at Supersonic Speeds
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42
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77952850763
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Investigation of an Inflatable Decelerator Attached to a 120-deg Conical Entry Capsule at Mach Numbers from 2.55 to 4.40
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-
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43
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44
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77952819579
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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
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-
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NASA Technical Note, NASA TN-D-4943
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45
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Static Longitudinal Aerodynamic Characteristics of Some Supersonic Decelerator Models at Mach Numbers of 2.30 and 4.63
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46
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33947113797
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Flight-Test Results from Supersonic Deployment of an 18-Foot-Diameter (5.49-meter) Towed Ballute Decelerator
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May
-
Mayhue, R.J., Eckstrom, C.V., "Flight-Test Results from Supersonic Deployment of an 18-Foot-Diameter (5.49-meter) Towed Ballute Decelerator," NASA Technical Memorandum, NASA TM-X-1773, May 1969.
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NASA Technical Memorandum, NASA TM-X-1773
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Mayhue, R.J.1
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47
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77952805300
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Investigation of an Attached Inflatable Decelerator with Mechanically Deployed Inlets at Mach Numbers from 2.25 to 4.75
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AEDC TR-69-132, June
-
Baker, D.C., "Investigation of an Attached Inflatable Decelerator with Mechanically Deployed Inlets at Mach Numbers from 2.25 to 4.75," ARO Inc. Technical Report, AEDC TR-69-132, June 1969.
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Baker, D.C.1
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48
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Mikulas Jr., M.M.1
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49
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77952831202
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Static Aerodynamic Characteristics, Pressure Distributions, and Ram-Air Inflation of Attached Inflatable Decelerator Models at Mach 3.0
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Deveikis, W.D.1
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50
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Drag Characteristics of Several Towed Decelerator Models at Mach 3
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May
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NASA Technical Note, NASA TN-D-5750
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51
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79955771765
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Deployment and Performance Characteristics of 5-Foot-Diameter (1.5 m) Attached Inflatable Decelerators from Mach Number 2.2 to 4.4
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August
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Bohon, H.L., Miserentino, R., "Deployment and Performance Characteristics of 5-Foot-Diameter (1.5 m) Attached Inflatable Decelerators from Mach Number 2.2 to 4.4," NASA Technical Note, NASA TN-D-5840, August 1970.
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52
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54
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October
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56
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Thermal and Stress Analysis of an Attached Inflatable Decelerator (AID) Deployed in the Mars and Earth Atmospheres
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GER-14939
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59
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Performance of a Ballute Decelerator Towed behind a Jet Airplane
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