Abstract
As Becker1 has recently pointed out, the ballistic entry vehicles of the ICBM program have almost achieved full maturity in the short span of about ten years. This has been accomplished through a combination of clearly defined requirements and a national research and development effort. With similar simple and clear requirements, the first manned orbital vehicles were developed by straightforward extensions of ICBM technology. This growth pattern now appears to be changing as the requirements for future systems become less clearly defined and, at the same time, become much more diverse and complex.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Becker, J. V.: Entry vehicles, Aeronautics and Aerospace Engineering, 1 (1963).
Clapp, R. T.: A Small State-of-the-Art Maneuverable Lifting Re-entry Vehicle, AIAA Paper 65–492, AIAA Second Annual Meeting, San Francisco, California (July 1965).
Love, E. S.: Manned lifting entry, Astronautics and Aeronautics, 5 (1966).
Eulberg, A. C.: A Translation of Manned Military Missions Into an Entry Vehicle Concept, AIAA Paper 65–488, AIAA Second Annual Meeting, San Francisco, California (July 1965).
Friedenthal, M. J.: Control of Re-entry From Orbit, Transactions of the 7 th Symposium on Ballistic Missile and Space Technology, vol. II (1962).
Galman, B. A.: Some Fundamental Considerations For Lifting Vehicles in Return From Satellite Orbit, Proceedings of the 4th AFBMD/STL Symposium on Ballistic Missile and Space Technology, vol. II (Pergamon Press, New York, 1961).
Low, G. M.: Nearly Circular Transfer Trajectories for Descending Satellites, NASA TR R-3 (1959).
Baker, J. M. and B. E. Baxter: Optimum deboost altitude for specified atmospheric entry angle, AIAA J. 1 (1963).
Detra, R. W., F. R. Riddell, and P. H. Rose: Controlled recovery of nonlifting satellites, ARS J. 30 (1960).
Galman, B. A.: Retrorocket alignment for maximum entry angle, ARS J. 32 (1962).
Esses, H.: Maximum ejection velocity for return from satellite orbits, ARS J. 29 (1959).
Royce, W.: The Altitude Oscillations of a Vehicle Re-entering the Atmosphere at a Constant Lift Coefficient, Space Technology Laboratories TN STL/TN-60–0000–09006 (14 January 1960).
Campbell, G. S.: Long period oscillations during atmospheric re-entry, ARS J.29 (July 1959).
Slye, R. E.: An Analytical Method for Studying the Lateral Motion of Atmospheric Entry Vehicles, NASA TN D-325 (September 1960).
Love, J. A.: A Drag Monitoring Guidance Scheme for a Lifting Re-entry Vehicle, Space Technology Laboratories TM STL/TM-60–0000–09047 (23 May 1960).
Assadourian, A. and D. C. Cheatham: Longitudinal Range Control During the Atmospheric Phase of a Manned Satellite Re-entry, NASA TN D-253 (May 1960).
Cheatham, D. C., J. W. Young, and J. M. Eggleston: The Variation and Control of Range Traveled in the Atmosphere by a High-Drag Variable-Lift Entry Vehicle, NASA TN D-230 (March 1960).
Eggleston, J. M. and J. W. Young: Trajectory Control for Vehicles Entering the Earth’s Atmosphere at Small Flight Path Angles, NASA Memorandum 1–19–59L (February 1959).
Eggers, A. J., J. H. Allen, and S. E. Neice, A Comparative Analysis of the Performance of Long-Range Hypersonic Vehicles, NACA TN-4046 (October 1957).
Wang, H. E. and R. S. Skulsky: Characteristics of lateral range during constant altitude glide, AIAA J. 1 (1963).
Haig, C. R. and L. D. Perlmutter: Use of lateral maneuver to extend the period of daylight landings from orbit, J. SR, 2 (1965).
Wallace, R. A. and W. A. Gray: Minimum lift-drag ratio required for global landing coverage, AIAA J. 1 (1963).
Wagner, W. E.: Roll modulation for maximum re-entry lateral range, J. SR, 2 (1965).
Wang, H. E. and S. T. Chu: Variable lift re-entry at superorbital and orbital speeds, AIAA J. 1 (1963).
Wang, H. E.: Motion of re-entry vehicles during constant-altitude glide, AIAA J. 3 (1965).
Loh, W. H. T.: Dynamics and Thermodynamics of Planetary Entry, Prentice-Hall, Inc., Englewood Cliffs, New Jersey, 1963.
Volgenan, E.: Boost Glide and Re-entry Guidance and Control, C. T. Leondes, Ed., McGraw-Hill Book Company, Chap. 10.
Boyle, E. J.: Recall and Return of a Manned Vehicle From Satellite Orbit, Proceedings of Symposium on Space Rendezvous Rescue and Recovery, vol. 16, (September, 1963 Advances in the Astronautical Sciences, Publication of American Astronautical Society).
Eggers, A. J. and T. J. Wong: Motion and heating of lifting vehicles during atmospheric entry, ARS J. 31 (1961).
Shen, Y. C.: Series solution of equations of re-entry vehicles with variable lift and drag coefficients, AIAA J. 1 (1963).
Allen, H. J. and A. J. Eggers: A study of the Motion and Aerodynamic Heating of Missiles Entering the Earth’s Atmosphere at High Supersonic Speeds, NACA TN-4047 (October 1957).
Love, E. S.: Factors influencing configuration and performance of multipurpose manned entry vehicles, J. SR., 1 (1964).
Spielberg, I. N. and C. B. Cohen: Janus: A manned orbital spacecraft with staged re-entry, J. SR., 2 (1965).
Love, E. S. and E. B. Pritchard: A Look at Manned Entry at Circular to Hyperbolic Velocities, Proceedings of the Second Manned Space Flight Meeting, Dallas, Texas (1963).
Eulberg, A. C.: A Translation of Manned Military Missions Into an Entry Vehicle Concept, AIAA Paper 65–488, AIAA Second Annual Meeting, San Francisco, California (July 1965).
Grahane, W. E.: Determination of Re-entry Performance of the M-2 Lifting Body Based on Aerodynamic Heating Considerations, Transactions of the 9th Symposium on Ballistic Missile and Space Technology, vol. II (1964).
Syvertson, C. A., et. al.: Some Considerations of the Performance of a Maneuverable, Lifting-Body Vehicle, Proceedings of Symposium on Space Rendezvous Rescue and Recovery, vol. 16, (September 1963 Advances in the Astronautical Sciences, Publication of American Astronautical Society).
Mathauser, E. E.: Research, Design Considerations, and Technological Problems of Structure for Winged Aerospace Vehicles, Proceedings of the NASA-University Conf. on the Science and Technology of Space Exploration, vol. 2 (Chicago, Illinois, 1962).
Baradell, D. L. and C. H. McLellan: Lateral Range and Hypersonic Lift Drag Ratio Requirements for Efficient Ferry Service from a Near Earth Manned Space Station. Paper presented at AIAA Second Manned Space Flight Meeting, Dallas, Texas (1963).
Nyland, F. S.: The Synergetic Plane Change for Orbiting Spacecraft, RAND Memorandum RM-3231-PR, Santa Monica, California (August 1962).
Bruce, R. W.: The Combined Aerodynamic Propulsive Orbital Plane Change Maneuver, Aerospace Corporation Report SSD-TDR-64–98, El Segundo, California (June 1964).
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1968 Springer Science+Business Media New York
About this chapter
Cite this chapter
Logan, J.G. (1968). Lifting Entry Concepts. In: Loh, W.H.T. (eds) Re-entry and Planetary Entry Physics and Technology. Applied Physics and Engineering, vol 3. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-50082-4_2
Download citation
DOI: https://doi.org/10.1007/978-3-642-50082-4_2
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-50084-8
Online ISBN: 978-3-642-50082-4
eBook Packages: Springer Book Archive