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Space trajectories

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• Trajectories (Mechanics)
• Astrodynamics
• Space flight
• Space vehicles

• Artificial satellites -- Atmospheric entry
• Artificial satellites -- Orbits
• Artificial satellites -- Tracking
• Orbital transfer (Space flight)
• Space vehicles -- Atmospheric entry
• Space vehicles -- Tracking
• Trajectory optimization

• Space vehicles -- Trajectories

• First compilation of papers on trajectory analysis and guidance theory. (Washington, Scientific and Technical Information Division. National Aeronautics and Space Administration; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1967), by Cambridge United States. Electronics Research Center (page images at HathiTrust; US access only)
• Simplified technique for determining pericynthion altitude of lunar orbits / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by L. Keith Barker and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Opportunities for ballistic missions to Halley's comet / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Robert W. Farquhar, William H. Wooden, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Tables of z functions for atmosphere entry analysis, ([Washington, U.S. Govt. Print. Off., 1962]), by Dean Roden Chapman and Arline K. Kapphahn (page images at HathiTrust)
• Ballistic mode Mercury orbiter mission opportunity handbook / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by G. R. Hollenbeck, P. S. Lewis, D. G. Roos, Ames Research Center, and Martin Marietta Corporation (page images at HathiTrust)
• Trajectories with constant tangential thrust in central gravitational fields, ([Washington, U.S. G.P.O.], 1960), by W. E. Moeckel (page images at HathiTrust)
• A preliminary study of some abort trajectories initiated during launch of a lunar mission vehicle / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by John M. Eggleston, William A. McGowan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On optimum transfer between two terminal points for minimum initial impulse under an arbitrary initial velocity vector / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by Fang Toh Sun and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Application of matched asymptotic expansions to lunar and interplanetary trajectories / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by J. E. Lancaster, Manned Spacecraft Center (U.S.), and McDonnell Douglas Astronautics Company-West (page images at HathiTrust)
• Development of a method for optimal maneuver analysis of complex space missions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Stewart F. McAdoo, G. S. Dawkins, Donald J. Jezewski, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Apollo experience report : evolution of the rendezvous-maneuver plan for lunar-landing missions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by James D. Alexander, Robert W. Becker, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Dynamics and column densities of small particles ejected from spacecraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by National Technical Information Service], 1974), by Robert J. Naumann and George C. Marshall Space Flight Center. Space Sciences Laboratory (page images at HathiTrust)
• Necessary conditions for optimal lunar trajectories with discontinuous state variables and intermediate point constraints / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by W. E. Miner, J. F. Landrus, Northrop Space Laboratories, and Electronics Research Center (U.S.) (page images at HathiTrust)
• Ballistic mode Mercury orbiter mission opportunity handbook extension / (Washington, D.C. : National Aeronautics and Space Administration, [1974]), by G. R. Hollenbeck, P. S. Lewis, P. C. Rockenbach, Ames Research Center, and Martin Marietta Corporation (page images at HathiTrust)
• Alternate multiple-outer-planet missions using a Saturn-Jupiter flyby sequence / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by John W. Young, Margery E. Hannah, and Langley Research Center (page images at HathiTrust)
• Effect of interplanetary trajectory options on a manned Mars aerobrake configuration / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Robert D. Braun, Lin C. Hartung, Richard W. Powell, and Langley Research Center (page images at HathiTrust)
• Theory of higher order optimum impulsive solutions / (Washington : National Aeronautics and Space Administration, 1971), by J. F. Andrus (page images at HathiTrust)
• Apollo experience report : real-time auxiliary computing facility development / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Charles E. Allday and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Simplified interplanetary guidance procedures using onboard optical measurements / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Harold A. Hamer, Katherine G. Johnson, and Langley Research Center (page images at HathiTrust)
• An analysis of atmospheric entry trajectories for manned and unmanned missions to the planet Venus (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Mark K. Craig, Ralph G. Gonzalez, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Hodograph analysis of the free-flight trajectories between two arbitrary terminal points / ([Washington] : National Aeronautics and Space Administration, [1965]), by Fang Toh Sun, University of Michigan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Application of statistical filter theory to the optimal estimation of position and velocity on board a circumlunar vehicle / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1962), by Gerald L. Smith, Leonard A. McGee, Stanley F. Schmidt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Explicit upper bounds for error propagation in the n-body field / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Albert Rosen, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
• Optimal three-dimensional resusable tug trajectories for planetary missions including correction for nodal precession / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1976), by Janos Borsody and Lewis Research Center (page images at HathiTrust)
• Single-thrust-period missions to Uranus for unmanned nuclear-electric propulsion systems / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Charles L. Zola and Lewis Research Center (page images at HathiTrust)
• The approximate analysis of zero-lift trajectories /, by C. P. Hoult and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
• Secondary errors and off-design conditions in optimal estimation of space vehicle trajectories / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Gerald L. Smith and Ames Research Center (page images at HathiTrust)
• Dynamics of atmospheric entry. (New York, McGraw-Hill, [1962]), by Robert Clifton Duncan (page images at HathiTrust)
• Computer program for beam transport problems / (Madison, Wisconsin : Midwestern Universities Research Association, 1962), by D. A. Swenson, U.S. Atomic Energy Commission, and Midwestern Universities Research Association (page images at HathiTrust)
• Environmental testing of the RFD-2 re-entry vehicle / (Albuquerque, N.M. : Sandia Corporation ; Springfield, Va. : Available from the Clearinghouse for Federal and Scientific Information, National Bureau of Standards, U.S. Department of Commerce, [1965]), by D. L. Krenz, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• The TTA generalized rigid body trajectory program for digital computer / (Albuquerque, New Mexico : Sandia Corporation, Springfield, Va. : Available from the Clearinghouse for Federal and Scientific Information, National Bureau of Standards, U.S. Department of Commerce, 1966), by J. A. F. Allensworth, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Analysis of missile trajectory measurement accuracy for data processing (Buffalo, Cornell Aeronautical Laboratory, 1961), by Thomas R. Benedict, George W. Bordner, and Rome Air Development Center. Control and Guidance Directorate (page images at HathiTrust)
• Earth-Venus trajectories. (Pasadena, 1962-63), by Jet Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Dispersal of reactor core materials by reentry processes; preliminary analysis, (Buffalo, 1962), by Cornell Aeronautical Laboratory and J. L. Beal (page images at HathiTrust)
• A method of approximating propellant requirements of low-thrust trajectories / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Charles L. Zola, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Round-trip trajectories with stopovers at both Mars and Venus / (Washington, D.C. : National Aeronautics and Space Administration, 1970), by Edward A. Willis and John A. Padrutt (page images at HathiTrust; US access only)
• A semigraphical method for a deorbit trajectory design study / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Richard N. Green, Sue W. Souders, William F. Hampshire, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Error analysis of several methods of determining vehicle position in earth-moon space from simultaneous onboard optical measurements / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Harold A. Hamer, Alton P. Mayo, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Midcourse and approach guidance requirements for simplified onboard control of moon-to-earth trajectories / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Harold A. Hamer, Katherine G. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Mathematical theory of the Goddard trajectory determination system / (Greenbelt, Maryland : Goddard Space Flight Center, [1976]), by Arthur J. Fuchs, C. E. Vélez, J. O. Cappellari, and Goddard Space Flight Center (page images at HathiTrust; US access only)
• Some efficient computation techniques including their application to time optimal trajectories from parking orbit / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by William B. Tucker and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Flight Mechanics/Estimation Theory Symposium 1990 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center ... Greenbelt, Maryland, May 22-24, 1990 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), by Flight Mechanics/Estimation Theory Symposium (1990 : Goddard Space Flight Center), Thomas Stengle, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of gravitational-model selection on accuracy of lunar orbit determination from short data arcs / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Harold A. Hamer, Katherine G. Johnson, and Langley Research Center (page images at HathiTrust)
• A study to evaluate STS heads-up ascent trajectory performance employing a minimum-Hamiltonian optimization strategy / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988), by Sujit Sinha and George C. Marshall Space Flight Center (page images at HathiTrust)
• Trajectory characteristics and heating of hypervelocity projectiles having large ballistic coeffients / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Michael E. Tauber and Ames Research Center (page images at HathiTrust)
• Capabilities and applications of the program to optimize simulated trajectories (POST) : program summary document / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by G. L. Brauer, R. Stevenson, D. E. Cornick, Martin Marietta Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Prediction of the pattern performance for the Aeroassist Flight Experiment (AFE) spacecraft / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by C. Yang, R. Torres, R. C. Rudduck, Ohio State University. ElectroScience Laboratory, and Langley Research Center (page images at HathiTrust)
• Reconstruction of the 1st space shuttle (STS-1) entry trajectory / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by J. T. Findlay, G. M. Kelly, M. L. Heck, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Analytical Mechanics Associates, and Langley Research Center (page images at HathiTrust)
• A study of guidance to reference trajectories for lifting reentry at supercircular velocity / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1963), by Rodney C. Wingrove, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On energy-optimal trajectories in three dimensions for the terminal phase of satellite rendezvous / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Terrance M. Carney, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A three-dimensional trajectory simulation using six degrees of freedom with arbitrary wind,. / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1961]), by Robert L. Jr James and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Three-dimensional trajectory analysis for round-trip missions to Mars / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Gerald Knip, Charles L. Zola, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Three-dimensional trajectory analysis for round-trip missions to Venus / (Washington : National Aeronautics and Space Administration, [1962]), by Charles L. Zola, Gerald Knip, and Lewis Research Center (page images at HathiTrust)
• Two-burn escape maneuvers with an intermediate coasting ellipse / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Edward A. Willis, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Linear theory of impulsive velocity corrections for space mission guidance / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Luigi S. Cicolani and Ames Research Center (page images at HathiTrust)
• Midcourse guidance for return from the moon to a geographically fixed landing site / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by John D. McLean, Luigi S. Cicolani, and Ames Research Center (page images at HathiTrust)
• A computational method for time-optimal space rendezvous / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Ernest S. Armstrong, Athena T. Markos, and Langley Research Center (page images at HathiTrust)
• A study of the effect of measurement errors upon a range controller for an entry vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Jack A. White and Langley Research Center (page images at HathiTrust)
• Round-trip trajectories to moons of Jupiter / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Roger W. Luidens, John Edgar, and Lewis Research Center (page images at HathiTrust)
• Theoretical relationships for meteoroid puncture experiments / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Charles C. Dalton and George C. Marshall Space Flight Center (page images at HathiTrust)
• Performance analysis of high-energy chemical stages for interplanetary missions / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Walter H. Stafford, Carmen R. Catalfamo, Sam H. Harlin, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Trajectories in the earth-moon space with symmetrical free return properties / (Washington : National Aeronautics and Space Administration, [1963]), by Arthur J. Schwaniger and George C. Marshall Space Flight Center. Aeroballistics Division. Future Projects Branch (page images at HathiTrust)
• Minimum fuel ascent from the lunar surface / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Albert E. Brown and Langley Research Center (page images at HathiTrust)
• Predictions on the characteristics of the minimal two-impulse orbital transfer under arbitrary terminal conditions by using the bounding trajectories / (Washington, D.C. : National Aeronautics and Space Administration, [1971]), by Fang Toh Sun (page images at HathiTrust)
• Parameter study of insertion conditions for lunar missions including various trajectory considerations / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Carl R. Huss, John P. Mayer, and Harold A. Hamer (page images at HathiTrust)
• Parametric performance analysis for interplanetery missions utilizing first-generation nuclear stages / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Walter H. Stafford, Carmen R. Catalfamo, Sam H. Harlin, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Return trajectories from the moon : some limits due to restrictions on entry range and landing lighting conditions / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Luigi S. Cicolani and Ames Research Center (page images at HathiTrust)
• A study of factors affecting the accuracy of the position fix for lunar trajectories / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Margery E. Hannah, Alton P. Mayo, and Langley Research Center (page images at HathiTrust)
• A study of ballistic reentry trajectories at a velocity of 50,000 feet per second (15,240 meters per second) / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by John T. Suttles, Lucille C. Coltrane, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Finite-thrust escape from and capture into circular and elliptic orbits / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Edward A. Willis and Lewis Research Center (page images at HathiTrust)
• Declination, radial distance, and phases of the moon for the years 1961 to 1971 for use in trajectory considerations / (Washington : National Aeronautics and Space Administration, [1961]), by Donald S. Woolston and Langley Research Center (page images at HathiTrust)
• Matched-conic solutions to round-trip interplanetary trajectory problems that insure state-vector continuity at all boundaries / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Victor R. Bond, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Minimum thrust for correcting Keplerian orbits with application to interplanetary guidance / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Frederick W. Boltz, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Second-order errors in linearized velocity corrections and their effects on the rate of convergence of iterative solutions / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by John D. McLean, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Numerical integration in a rigid-body trajectory program / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by John Edd Moore, United States National Aeronautics and Space Administration, and Aero-Astrodynamics Laboratory (George C. Marshall Space Flight Center) (page images at HathiTrust)
• Requirements of a Martian television experiment for three point-mass descent trajectories [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Friedrich O. Huck, Robert B. Spiers, Leonard P. Kopia, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Approximation to the statistics of midcourse velocity corrections / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Lawrence H. Hoffman, George R. Young, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Simple method of using onboard optical measurements to predict the orbit established after the lunar-ascent-transfer orbit / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by L. Keith Barker, Herman S. Fletcher, and Langley Research Center (page images at HathiTrust)
• Analysis of maximum range trajectories for rocket-propelled lunar flying vehicles in a uniform gravitational field / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by A. Gary Childs, Ernest S. Armstrong, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Minimal energy ballistic trajectories for manned and unmanned missions to Mercury, ([Washington] National Aeronautics and Space Administration, [1967]), by Laurence Albert Manning (page images at HathiTrust)
• Departure trajectories for interplanetary vehicles / (Washington : National Aeronautics and Space Administration, [1959]), by W. E. Moeckel and Lewis Research Center (page images at HathiTrust)
• Tracking systems, their mathematical models and their errors. (Washington, [D.C.] : National Aeronautics and Space Administration, 1962), by F. O. Vonbun, W. D. Kahn, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
• A lighting strategy for lunar orbiter mission design / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Friedrich O. Huck, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Guidance and control during direct-descent parabolic reentry / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Edwin C. Foudriat, Rodney C. Wingrove, United States National Aeronautics and Space Administration, Ames Research Center, Langley Research Center, and D.C.) NASA-Industry Apollo Technical Conference (1961 : Washington (page images at HathiTrust)
• Preliminary determination of spacecraft trajectories using on-board optical measurements / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by John D. McLean, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Optimal reusable-tug and expendable-kickstage trajectories for high-energy planetary missions including correction for nodal precession / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Janos Borsody and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The basic mathematical concepts of rocket flight and earth satellites. (Chadron, Nebraska State Teachers College, [1959]), by Lenora D. Briggs (page images at HathiTrust)
• Trajectory optimization for an Apollo-type vehicle under entry conditions encountered during lunar return / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by John W. Young and Robert L. Smith (page images at HathiTrust; US access only)
• A manual method for control of the thrust axis during planar ascent from the lunar surface to a circular orbit / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1966), by Herman S. Fletcher, L. Keith Barker, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Orbital flight handbook (Washington, Office of Scientific and Technical Information] National Aeronautics and Space Administration, [1963]), by Martin Company. Space Systems Division, Donald Kraft, George Townsend, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Sequential processing techniques for trajectory estimation / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by C. G. Pfeiffer, TRW Systems Group, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Some optimal branched trajectories / (Redondo Beach, Calif. : TRW Systems Group ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1969), by Joseph D. Mason (page images at HathiTrust; US access only)
• Multisegmented optimal trajectories / (Washington : NASA ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Thomas L. Vincent and University of Arizona (page images at HathiTrust; US access only)
• A theoretical study of meteoric trajectories and processes, including examination of the incidence and characteristics of photographic meteors by reduction of about 600 data points / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Annette Posen and Richard E. McCrosky (page images at HathiTrust; US access only)
• Equations for determining vehicle position in earth-moon space from simultaneous onboard optical measurements / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Alton P. Mayo, Margery E. Hannah, Harold A. Hamer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

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