Space trajectoriesSee also what's at your library, or elsewhere.
Broader terms:Narrower terms:Used for:- Space vehicles -- Trajectories
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Filed under: Space trajectories- Dynamics of atmospheric entry. (McGraw-Hill, 1962), by Robert Clifton Duncan (page images at HathiTrust)
- The basic mathematical concepts of rocket flight and earth satellites. (Nebraska State Teachers College, 1959), by Lenora D. Briggs (page images at HathiTrust)
- Analysis of missile trajectory measurement accuracy for data processing (Cornell Aeronautical Laboratory, 1961), by Thomas R. Benedict, George W. Bordner, and Rome Air Development Center. Control and Guidance Directorate (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 study to evaluate STS heads-up ascent trajectory performance employing a minimum-Hamiltonian optimization strategy (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Sujit Sinha and George C. Marshall Space Flight Center (page images at HathiTrust)
- Effect of interplanetary trajectory options on a manned Mars aerobrake configuration (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Robert D. Braun, Lin C. Hartung, Richard W. Powell, and Langley Research Center (page images at HathiTrust)
- Trajectory characteristics and heating of hypervelocity projectiles having large ballistic coeffients (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Michael E. Tauber and Ames Research Center (page images at HathiTrust)
- NASA CR-1360 (National Aeronautics and Space Administration ;, 1969), by C. G. Pfeiffer, TRW Systems Group, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Predictions on the characteristics of the minimal two-impulse orbital transfer under arbitrary terminal conditions by using the bounding trajectories (National Aeronautics and Space Administration, 1971), by Fang Toh Sun (page images at HathiTrust)
- Theory of higher order optimum impulsive solutions (National Aeronautics and Space Administration, 1971), by J. F. Andrus (page images at HathiTrust)
- Analysis of the free-flight trajectories between two arbitrary terminal points (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)
- Reconstruction of the 1st space shuttle (STS-1) entry trajectory (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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 theoretical study of meteoric trajectories and processes, including examination of the incidence and characteristics of photographic meteors by reduction of about 600 data points (National Aeronautics and Space Administration, 1967), by Annette Posen and Richard E. McCrosky (page images at HathiTrust)
- Parameter study of insertion conditions for lunar missions including various trajectory considerations (National Aeronautics and Space Administration, 1961), by Carl R. Huss, John P. Mayer, and Harold A. Hamer (page images at HathiTrust)
- Trajectories with constant tangential thrust in central gravitational fields (U.S. G.P.O.], 1960), by W. E. Moeckel (page images at HathiTrust)
- NASA TR R-151 (National Aeronautics and Space Administration ;, 1963), by Rodney C. Wingrove, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Trajectory optimization for an Apollo-type vehicle under entry conditions encountered during lunar return (National Aeronautics and Space Administration, 1967), by John W. Young and Robert L. Smith (page images at HathiTrust)
- NASA TR R-135 (National Aeronautics and Space Administration ;, 1962), by Gerald L. Smith, Leonard A. McGee, Stanley F. Schmidt, 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 (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,. (National Aeronautics and Space Administration :, 1961), by Robert L. Jr James and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-3681 (National Aeronautics and Space Administration :, 1966), by Herman S. Fletcher, L. Keith Barker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-3400 (National Aeronautics and Space Administration ;, 1966), by Charles L. Zola, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-2691 (National Aeronautics and Space Administration, 1965), by William B. Tucker and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Three-dimensional trajectory analysis for round-trip missions to Mars (National Aeronautics and Space Administration :, 1962), by Gerald Knip, Charles L. Zola, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Declination, radial distance, and phases of the moon for the years 1961 to 1971 for use in trajectory considerations (National Aeronautics and Space Administration, 1961), by Donald S. Woolston and Langley Research Center (page images at HathiTrust)
- Optimal three-dimensional resusable tug trajectories for planetary missions including correction for nodal precession (National Aeronautics and Space Administration ;, 1976), by Janos Borsody and Lewis Research Center (page images at HathiTrust)
- NASA TN D-4811 (National Aeronautics and Space Administration :, 1968), by L. Keith Barker and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Round-trip trajectories with stopovers at both Mars and Venus (National Aeronautics and Space Administration, 1970), by Edward A. Willis and John A. Padrutt (page images at HathiTrust)
- NASA TN D-4801 (National Aeronautics and Space Administration :, 1968), by Richard N. Green, Sue W. Souders, William F. Hampshire, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-4791 (National Aeronautics and Space Administration :, 1968), by Thomas E. Walton, Brian J. O'Hare, William G. Witte, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Simple method of using onboard optical measurements to predict the orbit established after the lunar-ascent-transfer orbit (National Aeronautics and Space Administration ;, 1970), by L. Keith Barker, Herman S. Fletcher, and Langley Research Center (page images at HathiTrust)
- Simplified interplanetary guidance procedures using onboard optical measurements (National Aeronautics and Space Administration ;, 1972), by Harold A. Hamer, Katherine G. Johnson, and Langley Research Center (page images at HathiTrust)
- Apollo experience report : evolution of the rendezvous-maneuver plan for lunar-landing missions (National Aeronautics and Space Administration ;, 1973), by James D. Alexander, Robert W. Becker, and Lyndon B. Johnson Space Center (page images at HathiTrust)
- Minimal energy ballistic trajectories for manned and unmanned missions to Mercury (National Aeronautics and Space Administration, 1967), by Laurence Albert Manning (page images at HathiTrust)
- NASA TN D-1604 (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)
- NASA TN D-4501 (National Aeronautics and Space Administration ;, 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 (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)
- Dynamics and column densities of small particles ejected from spacecraft (National Aeronautics and Space Administration ;, 1974), by Robert J. Naumann and George C. Marshall Space Flight Center. Space Sciences Laboratory (page images at HathiTrust)
- An analysis of atmospheric entry trajectories for manned and unmanned missions to the planet Venus (National Aeronautics and Space Administration ;, 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)
- Error analysis of several methods of determining vehicle position in earth-moon space from simultaneous onboard optical measurements (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)
- Alternate multiple-outer-planet missions using a Saturn-Jupiter flyby sequence (National Aeronautics and Space Administration ;, 1973), by John W. Young, Margery E. Hannah, and Langley Research Center (page images at HathiTrust)
- Single-thrust-period missions to Uranus for unmanned nuclear-electric propulsion systems (National Aeronautics and Space Administration ;, 1973), by Charles L. Zola and Lewis Research Center (page images at HathiTrust)
- NASA TN D-6343 (National Aeronautics and Space Administration ;, 1971), by Harold A. Hamer, Katherine G. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- NASA TN D-6551 (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 1976), by Janos Borsody and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Opportunities for ballistic missions to Halley's comet (National Aeronautics and Space Administration ;, 1977), by Robert W. Farquhar, William H. Wooden, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- A preliminary study of some abort trajectories initiated during launch of a lunar mission vehicle (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)
- Computer program for beam transport problems (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 (Sandia Corporation ;, 1965), by D. L. Krenz, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
- Orbital flight handbook (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)
- The approximate analysis of zero-lift trajectories (Bedford, Massachusetts : Geophysics Research Directorate, Air Force Cambridge Research Center, 1959., 1959), by C. P. Hoult and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
- Approximate transfer functions for flexible-booster-and-autopilot analysis (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by David R. Lukens, George T. Broucek, ALfred F. Schmitt, United States. Air Force. Air Research and Development Command, and Wright Air Development Division (page images at HathiTrust)
- Space vehicle ephemeris and differential correction program unified theory. (Air Force Command and Control Development Division, Air Research and Development Command, U.S. Air Force, Laurence G. Hanscom Field, 1960), by Ford Motor Company. Aeronutronic. Astrodynamics Dept and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
- On take-off from circular orbit by small thrust (Polytechnic Institute of Brooklyn, Department of Aerospace Engineering and Applied Mechanics, 1962), by Lu Ting, Sherwood Brofman, United States. Air Force. Office of Aerospace Research, and Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
- Optimizing interplanetary trajectories with deep space maneuvers (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), by John Navagh, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, and Langley Research Center (page images at HathiTrust)
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