11 - Supersonic parachutes Lingard.pdf

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Cp Parachute surface pressures 2 1.5 1 0.5 -0.5 vent 0 skirt 0 1 2 3 4 5 6 Mach 3 no lines (internal) Mach 1.08 no lines (internal) Mach 3 with lines (internal) Mach 1.08 with lines (internal) Mach 3 no lines (external) Mach 1.08 no lines (external) Mach 3 with lines (external) Mach 1.08 with lines (external)
<strong>Supersonic</strong> parachute behavior
Page 1 and 2: Parachute Seminar 3rd International
Page 3 and 4: Requirements high drag to weight ra
Page 5 and 6: Ribbon parachute drag coefficient
Page 7 and 8: Supersonic parachute behavior Cd 0.
Page 9 and 10: Supersonic Flow Compressibility Hig
Page 11 and 12: Flow around a hollow hemisphere Mac
Page 13 and 14: Hemisflo - M 1.9 Shock waves
Page 15: Flow around a hollow hemisphere and
Page 19 and 20: Flow around a disk-gap disk gap-ban
Page 37 and 38: Wake effects M Forebody Shock 1 Sho
Page 39 and 40: Ribbon flutter modified pressure di
Page 41 and 42: Conical Ribbon Parachute
Page 43 and 44: Hemisflo Parachute More refined sha
Page 45 and 46: Supersonic-X Supersonic X parachute
Page 47 and 48: Disk-Gap Disk Gap-Band Band tested
Page 49 and 50: Hermes Testing Test decelerators: s
Page 51 and 52: Ribbon parachute drag coefficient
Page 53 and 54: Drag coefficient vs M
Page 55 and 56: Huygens DGB main ogive wake Cd 0.75
Page 57 and 58: Galileo testing - transonic drag lo
Page 59 and 60: Drag summary Conical ribbon - effec
Page 61 and 62: Stability vs M
Page 63 and 64: Inflation distance as function of M
Page 65 and 66: Aerodynamic Heating stagnation temp
Page 67 and 68:
Aerodynamic Heating high temperatur
Page 69 and 70:
Design guide 2 sometimes a multi-st
Page 71 and 72:
Design guide 4 if aerodynamic heati
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11 - Supersonic parachutes Lingard.pdf

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