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NASA TN D-6240

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National Aeronautics and Space Administration, 1971 - Conical shells - 28 pages

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Common terms and phrases

angles of 13.5 appendix atmosphere for three atmosphere Max atmosphere Min Hp atmosphere with maximum average density scale calculated drag coefficient coefficient with Mach conical aeroshell curve fits density near surface density scale height DRAG AND TRAJECTORIES effect for 0E entry flight-path angles entry spacecraft Entry velocity effect equilibrium thermodynamic five model atmospheres five model Mars flight-path angle effect free-stream gas constant Hp atmosphere atmosphere Hp model atmosphere interpolation parameter kilometers 295 km/sec Langley Research Center linear interpolation m/sec ft/sec Mach number mass trajectory equations Max Hp atmosphere Max Hp model Max pg Mean model atmosphere minimum average density model Mars atmospheres molecular mass NASA TN point mass trajectory real-gas drag coefficient real-gas effects shock density ratio slug/ft2 specific heats standard point mass temperature thermodynamic properties three entry flight-path three entry velocities undissociated gas mixture unit mass Variation of calculated variation of drag velocities and three velocities of 4.27

Bibliographic information

QR code for NASA TN D-6240
TitleNASA TN D-6240
Volume 6240 of NASA technical note
AuthorsDennis O. Allison, Percy J. Bobbitt, United States. National Aeronautics and Space Administration, Langley Research Center
PublisherNational Aeronautics and Space Administration, 1971
Length28 pages
SubjectsConical shells
Drag (Aerodynamics)
Gases, Real
Space vehicles
Trajectory optimization
  
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