A survey of aeroassisted orbit transfer
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^arzecha, L.W. "Performance and Design Considerations for Maneuvering Space Vehicles,*' IAS paper 60-59, 1960.
London H. S., 1961, IAS 29th Annual Meeting
Nyland F.S., 1962, The Synergetic Plane Change for Orbiting Spacecraft
Bell N., 1963, ASD-TDR-63-693
Nyland F.S., 1963, Proceedings of 5th International Symposium on Space Technology and Science
Cuadra E., 1965, AIAA Paper, 341
Hunter J.W., 1965, Air University Review, 16, 109
Paine J.P., 1966, AIAA Paper, 698
Clauss J.S. Jr., 1967, AIAA Paper
Nyland F.S., 1967, Considerations of Applying Continuous Thrust During Syriergetic Plane Changing
16Bonner, M.M. "Minimum Fuel Trajectories for the Synergetic Plane Change Maneuver," Ph.D. Thesis,University of Michigan, Ann Arbor, 1967.
Tramonti L., 1967, Saturn V/Apollo and Beyond, National Symposium, Transactions, Huntsville, Ala., 2
Nyland F.S., 1968, American Astronautical Society and AIAA Astrodynamics Specialist Conference, Jackson, Wyo.
Dickmanns E.D., 1969, Dr.-Ing. Dissertation, Rheinisch-Westfaelische Technische Hochschule
Dickmanns E.D., 20th Congress of the International Astronautical Federation, Mar Del Plata, Argentina, Oct.1969
Wuest W., 1971, 9th Course in Space Flight Techniques Proceedings, Universitaet Gottingen, Gottingen, FRG, 1
Tramonti L., 1972, NASA Langley Research Center Space Shuttle Aerothermodynamics Technical Conference, 4, 1439
Dickmanns E.D., 24th International Astronautical Congress, Baku, USSR, Oct.1973
26Dickmanns, E.D. "The Effect of Finite Thrust and Heating Constraints on the Synergetic Plane Maneuver for a Space Shuttle Orbiter-Class Vehicle," NASA TN-D-7211, Oct.1973.
27Spathopoulos, T. "A Guidance Scheme for the Synergetic Trajectory Turning Maneuver," Ph.D. Thesis, Technische Universitaet,Munich, FRG, March 1975.
Dickmanns E.D., 1980, FRG
Aerodynamic Design Data Book, 1
Joosten, B.K. and Pierson, B.L. "Minimum Fuel Aerodynamic Orbital Plane Change Maneuvers," AIAA Paper 81-0167, Jan.1981.
Program Review, Rockwell International, Rept. NA-, 81, 1981
Lichtenstein J.H., 1965, NASA TN D-2837
Bano R.L., 1966, Performance Data for Mars Capture and Lander Vehicles Using Aero-braking
Repic E.M., 1968, AIAA Paper
Meston R.D., 1968, Technological Requirements Common to Manned Planetary Missions
Johnson W.E., 1968, AAS Paper
Eliasberg P.E., Proceedings of Astronautical Research 1970, 21st International Astronautical Federation Congress, Konstanz, FRG, Oct.1970, 48
Eysmont N.A., 1974, Applied Problems of Space Ballistics, Scientific Translation Service, Santa Barbara, Calif., NASA-TT-F-15412, 13
Barbieri R.W., 1975, AAS Paper
Okhotsimskii D.E., 1977, KosmicheskieIssledovaniia, 15, 336
Okhotsimskii D.E., 1977, Cosmic Research, 15, 287
Cruz M.I., 1979, AAS Paper
Cruz M.I., 1979, IAF 30th International Astronautical Congress
54French, J.R.,and Uphoff, C.W."Aerobraking for Planetary Missions," AAS Paper 79-286, Nov.1979.
French J.R., 1980, Astronautics and Aeronautics, 18, 48
General Electric Co. and Jet Propulsion Lab., Pasadena, Calif., NASA CR-164160, Oct.1980., 2
Generic Aerocapture Atmospheric Entry, 1980, Pasadena, Calif. NASA CR-164161
Tang C.C.H., 1981, AAS Paper
Kerridge S.J., 1981, ASS Paper
Dallas S.S., 1981, AIAA Paper
Mease K.D., 1982, AIAA Paper
Kostoff R.N., 1957, Bellcomm
Kostoff R.M., 1971, Bellcomm
Corso C.J., 1972, Space Tug Aerobraking Study, 1
Corso C.J., 1972, Technical, 2
Hendricks W.L., 1972, Nonequilibrium and Equilibrium Radiation to the Space Tug from the Shock Layer
Andrews D.G., 1973, Feasibility and Tradeoff Study of an Aeromaneuvering Orbit-to-Orbit Shuttle (AMOOS)
Ketter F.C. Jr., 2042, Results of Test to Determine the Aerodynamic Characteristics of Two Potential Aeromaneuvering Orbit-to-Orbit Shuttle (AMOOS) Vehicle Configurations in the NASA Ames 3.5-Foot Hypersonic Wind Tunnel
White J., 1974, Feasibility and Tradeoff Study of an Aeromaneuvering Orbit-to-Orbit Shuttle (AMOOS)
Render J.J., 1975, NASA TM X-74638
Render J.J., 1975, AAS Paper
Hethcoat J.P., 1976, IAF 27th International Astronautical Congress, Anaheim, Calif.
80Chambers, R.J. "Navigation Accuracy Requirements of Aeromaneuvering Space Vehicles," M.S. Thesis,Air Force Institute of Technology, Wright-PattersonAFB, Dayton, Ohio,March 1977.
Program Development NASA, 1977, NASA TM, 73394
Boyland R.E., 1979, Manned Geosynchronous Mission Requirements and Systems Analysis Study
1980, The Boeing Company. Seattle. Rept. D, 180, 1
Rocketdyne, 1981, Rocketdyne, Canoga Park, Calif., NASA CR-161688
1981, General Dynamics-Convair Div., Rept. GDC-ASP-, 80, 1
Walberg G. D., 1981, 32nd International Astronautical Federation Congress
Cruz M.I., 1982, AIAA Paper
Davies C.B., 1983, AIAA Paper
Menees G.P., 1983, AIAA Paper
Vinh N.X., 2092, AIAA Paper
Cruz M.I., 2093, AIAA Paper
Mease K.D., 2094, AIAA Paper
Cervisi R.T., 2095, AIAA Paper
Ikawa H., 2096, AIAA Paper
Gamble J.D., 1983, AIAA Paper
Andrews D.G., 1983, Vols. I and II
Park C., 1983, AIAA Paper
Menees G.P., 1984, AIAA Paper, 84
Powell R.W., 1984, AIAA Paper
Rehder J.J., 1984, AIAA Paper
Talay T.A., 1984, AIAA Paper
Morris W.D., 1984, AIAA Paper
Balakrishnah A., 1984, AIAA Paper
Martin F.W. Jr., 1984, AIAA Paper
Lombard C.K., 1984, AIAA Paper
Menees G.P., 1984, AIAA Paper
Pitts W.C., 1984, AIAA Paper
Lee J.H., 1984, AIAA Paper
Park C., 1984, AIAA Paper
Paris S.W., 2041, AIAA Paper
Miller C.G., 1984, AIAA Paper
Woods W.C., 1984, AIAA Paper
Andrews D.G., 1984, System Technology Analysis of Aeroassisted Orbital Transfer Vehicle (Low Lift/Drag)