More about Redstone Arsenal (Ala.):
| | Books about Redstone Arsenal (Ala.) --
Books by Redstone Arsenal (Ala.) Books about Redstone Arsenal (Ala.):
3 additional books about Redstone Arsenal (Ala.) in the extended shelves: Survey of available high pressure pneumatic components : (5,000 PSI and UP) (Redstone Arsenal, Alabama : Research Branch, Redstone Scientific Information Center, 1965., 1965), by Herbert H. Hoop, Pneumatics, George C. Marshall Space Flight Center, U.S. Army Aviation and Missile Command, Battelle Memorial Institute, U.S. Atomic Energy Commission, and Redstone Scientific Information Center (page images at HathiTrust)
Housing demand at Redstone Arsenal. Hearing ... Eighty-fourth Congress, Second Session, February 27, 1956. (U.S. Govt. Print. Off., 1956), by United States Senate Committee on Banking and Currency (page images at HathiTrust)
Historical origins of the George C. Marshall Space Flight Center. (Historical Office, Office of Management Services, George C. Marshall Space Flight Center, National Aeronautics and Space Administration, 1960), by David S. Akens (page images at HathiTrust)
Books by Redstone Arsenal (Ala.): Books in the extended shelves: Redstone Arsenal (Ala.): Aerodynamic analysis of a "flex" fin concept (Redstone Arsenal, Alabama ; U.S. Army Missile Command, System Simulation and Development Directorate, Research, Development, and Enginering Center, 1987., 1987), also by George A. Sanders and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Aerodynamic characteristics of a series of bodies with and without tails at Mach Numbers from 0.8 to 3.0 and angles of attack from 0 to 45 degrees (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by Jimmie N. Derrick, Gary C. Winn, Donald J. Spring, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Aerodynamic characteristics of wraparound fins mounted on bodies of revolution and rheir influence on the missile static stability at Mach numbers from 0.3 to 1.3 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by Calvin Wayne Dahlke, Joseph C. Craft, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Aerodynamic Data Base User's Guide (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Systems Simulation Directorate, Technology Laboratory, 1979., 1979), also by George M. Landingham and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Aerodynamic performance of missile configurations at transonic speeds including the effects of a jet plume (Redstone Arsenal, Alabama : U.S. Army Missile Command, 1976., 1976), also by Jain-Ming Wu, U. Uchiyama, Trevor H. Moulden, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Aerodynamic prediction methods, RDF-129 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorate, Research, Development, and Engineering Center, 1989., 1989), also by J. L. Sims, Robert H. Carnesi, L. G. Mendel, John F. Stalnaker, United States. Army. Missile Command, and Georgia Tech Research Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Aerodynamics of longitudinally supported ring tail configurations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Aeroballistics Directorate, 1971., 1971), also by Calvin Wayne Dahlke and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): An approach to experimental investigation of jet plume effects on missile aerodynamics (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1982., 1982), also by George M. Landingham and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Approximate determination of jet contours near the exit of axially symmetrical nozzles as a basis for plume modeling (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Directorate for Research, Development, Enginering and Missile Systems Laboratory, 1972., 1972), also by H. H. Korst and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Army aviation : foundations of the modern fleet (Redstone Arsenal, Alabama : Program Executive Office, Aviation, Public Affairs Office, 2013, 2013) (page images at HathiTrust) Redstone Arsenal (Ala.): Army Ballistic Missile Agency report (Army Ballistic Missile Agency, Redstone Arsenal., in the 20th century), also by Army Ballistic Missile Agency (page images at HathiTrust) Redstone Arsenal (Ala.): An assessment of the Martin-Marietta high angle of attack aerodynamic methodology for body tail missiles (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by Donald J. Spring, Gary C. Winn, Jimmie N. Derrick, and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): Computer program for estimating stability derivatives of missile configurations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by William D. Washington and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Computer program for estimating stability derivatives of missile configurations : users manual (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1982., 1982), also by George A. Sanders and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Correlation of viscous effects and comparison between experimental and theoretical distribution of potential normal force and pitching moment for bodies of revolution at supersonic speeds (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research and Development Directorate, Advanced Systems Labortory, 1967., 1967), also by William David Washington and United States. Army. Missile Command. Research and Development Directorate (page images at HathiTrust) Redstone Arsenal (Ala.): CRAFT time dependent analysis of a missile with lateral control jet (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorate, Research, Development, and Engineering Center, 1992, 1992), also by Ashvin Hosangadi, Brian J. York, United States. Army. Missile Command, and Science Applications International Corporation (page images at HathiTrust) Redstone Arsenal (Ala.): Effect of forebody wing strakes on enhancing performance of a typical body-wing-tail missile configuration at Mach 2.0 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1980., 1980), also by Pamela K. Alstott, William David Washington, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Effect of missile nose length and shape on fin effectiveness (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1970., 1970), also by Donald V. Rubin, Wiley Pettis, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): The effect of wrap-around fins on aerodynamic stability and rolling moment variations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1973., 1973), also by C. W. Dahlke, J. C. Craft, and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): The effectiveness of canards for roll control. (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by James R Burt and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation of a transverse jet ejecting from a flat plate into a subsonic free stream (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1970., 1970), also by Troy A. Street and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation of base pressure on a body of revolution at high thrust levels and free stream Mach numbers of 1.5 to 2.87 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1970., 1970), also by Joseph C. Craft, Charles E. Brazzel, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation of downstream flow-field properties behind a forward located sonic jet injected into transonic freestream from a body of revolution (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1968., 1968), also by Calvin Wayne Dahlke and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation of downstream flow-field properties behind a sonic jet injected into transonic free stream from a body of revolution : Series II (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1969., 1969), also by Calvin Wayne Dahlke and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation of the aerodynamic characteristics of nose mounted canard configurations at supersonic Mach numbers (1.5 through 4.5) (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by James R Burt, Chryler Corporation, and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation of the aerodynamic characteristics of several nose-mounted canard configurations at transonic Mach numbers (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1974., 1974), also by James R Burt, Chrysler Corporation, and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation of the interference effects due to a lateral jet issuing from a body of revolution over the Mach number range of 0.8 to 4.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1968., 1968), also by Donald J. Spring and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): An experimental investigation using a normal jet plume simulator to determine jet plume effects on a long slender rocket configuration at Mach numbers from 0.2 to 1.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, 1977., 1977), also by James H Henderson, G. Batiuk, Calvin Wayne Dahlke, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Experimental study on high subsonic turbulent flow incipient separation (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by Jain-Ming Wu, Hideki Kuwano, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): An exploratory investigation on reducing supersonic missile drag by fluid injection into a turbulent boundary layer (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by Donald Rubin and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): Free air plume overpressure for 2.75 inch rocket motors Mark 40 and Mark 66 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Ground Equipment and Missile Structures Directorate, 1980., 1980), also by Robert Bergman, Donald Davis, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Grid fin analysis. Vol. 1 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorate, Research, Development, and Engineering Center, 1994, 1994), also by John E. Burkhalter, Todd Michael Leleux, United States. Army. Missile Command, and Auburn University (page images at HathiTrust) Redstone Arsenal (Ala.): Guide to the operation of the MIRADCOM/UTSI computer program for plume induced sepertion at transonic speeds (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, Technology Laboratory, 1977., 1977), also by D. J. Spring, Trevor H. Moulden, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): An investigation of flow and stability characteristics for a body of revolution with fins and flare in presence of Plume induced separation at Mach numbers 0.7 to 1.4 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Direcorate, Technology Laboratory, 1977., 1977), also by Calvin Wayne Dahlke and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Investigation of jet plume effects on the longitudinal stability characteristics of a body of revolution with various fin configurations at Mach numbers from 0.2 to 2.3 : normal jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by James H. Henderson and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): An investigation of jet plume effects on the stability characteristics of a body of revolution in conjunction with fins of various geometry and longitudinal positions at transonic speeds (sting-mounted model with normal jet plume simulator) (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1975., 1975), also by James H Henderson and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Investigation of plume induced separation on a full-size missile at supersonic velocities (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1980., 1980), also by T. A. Martin and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): An investigation of streamwise body-fin gaps as a means of alleviating the adverse plume effects on missile longitudinal stability. (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1977., 1977), also by James H. Henderson and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): An investigation of the aerodynamic stabilizing effectiveness of several split flare afterbody configurations in the presence of an underexpanded jet plume at transonic Mach numbers (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, Technology Laboratory, 1978., 1978), also by James R. Burt and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Investigation of the effect of low thrust levels on the base pressure of a cylindrical body at supersonic speeds (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research and Development Directorate, Advanced Systems Labortory, 1970., 1970), also by T. A. Martin, C. E. Brazzel, and United States. Army. Missile Command. Research and Development Directorate (page images at HathiTrust) Redstone Arsenal (Ala.): An investigation of the effectiveness of several devices in simulating a rocket plume at free stream Mach numbers 0.9 to 1.2 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971), also by James Robert Burt and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Inviscid flow analysis on body of revolution with slender cruciform canted delta fins at small angle of incidence (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1975., 1975), also by N. Uchiyama, J. M. Wu, University of Tennessee (System). Space Institute, and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): Jet interaction control effectiveness for subsonic and supersonic flight : final report (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1969., 1969), also by Louis A. Cassel, James M. Kelso, Clark W. Bullard, Norbert A. Durando, United States. Army. Missile Command, and McDonnell Douglas Astronautics Company-West (page images at HathiTrust) Redstone Arsenal (Ala.): Missile dynamics equations for guidance and control modeling and analysis (Redstone Arsenal, Alabama : U.S. Army Missile Command, 1984., 1984), also by Philip N. Jenkins and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Modified Barrowman Method with applications to the Optical Deep Attack Missile Systems and Precision Deep Attack Missile Systems vehicles (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research Directorate, Research, Development, and Enginering Center, 1989., 1989), also by Charles E. Hall and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Normal force effectiveness of several fin planforms with streamwise gaps at Mach numbers of 0.8 to 5.0 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research and Development Directorate, Advanced Systems Laboratory, 1970., 1970), also by C. W. Dahlke, W. Pettis, and United States. Army. Missile Command. Research and Development Directorate (page images at HathiTrust) Redstone Arsenal (Ala.): An oil flow study of a sonic reaction jet ejecting from a body of revolution into a free stream of Mach number range 1.75 to 4.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research and Development Directorate, Advanced Systems Labortory, 1970., 1970), also by Troy A. Street and United States. Army. Missile Command. Research and Development Directorate (page images at HathiTrust) Redstone Arsenal (Ala.): An outline of methods applicable to viscous fluid flow problems (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971), also by Trevor H. Moulden, Jain-Ming Wu, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Preliminary review of approximate calculative methods for transonic flow around bodies of revolution (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by Jain-Ming Wu, Kinya Aoyama, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Pressure distributions for axisymmetric bodies with discontinuous curvature in transonic flow (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1970., 1970), also by Jain-Ming Wu, Kinya Aoyama, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Properties and tables of generalized rocket functions, for use in the theory of rockets with a constant slow spin,. ([Ithaca, N.Y.], 1953), also by J. Barkley Rosser and Robert John Walker (page images at HathiTrust) Redstone Arsenal (Ala.): Shielding for nuclear rockets (Oak Ridge, Tennessee : Oak Ridge National Laboratory, 1954., 1954), also by James E. Norman, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust) Redstone Arsenal (Ala.): Solution of transient heat transfer problems for flat plates, cylinders, and spheres by finite-difference methods (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Directorte of Research and Development, 1965., 1965), also by W. G. Burleson, R Eppes, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 0.5 to 1.3 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1972., 1972), also by John E. Vaughn, Calvin Wayne Dahlke, Joseph C. Craft, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 1.6 to 2.86 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by John E. Vaughn, Calvin Wayne Dahlke, Joseph C. Craft, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): A study of various slender and non-slender fin-body combinations of missile configurations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1976., 1976), also by N. Uchiyama, Jain-Ming Wu, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): A study to determine the accuracy of two computer programs in predicting hinge moments for all movable tail fins on missile bodies (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Systems Simulation and Development Directorte, 1983., 1983), also by George A. Sanders and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): A summary of aerodynamic characteristics for wrap-around fins from Mach 0.3 to 3.0 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, 1977., 1977), also by James A. Humphrey, Calvin Wayne Dahlke, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): A summary of jet plume effects on the stability characteristics of a body of revolution with various fin configurations at Mach numbers from 0.2 to 2.3 : normal jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1976., 1976), also by George Batiuk, James H. Henderson, and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): Supersonic flow around right circular cones, tables for zero angle of attack (Redstone Arsenal, Alabama ; U.S. Army Ballistic Missile Agency, Aerodynamics Analysis Branch, Aeroballistics Laboratory, 1960., 1960), also by Joseph L. Sims and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Theoretical analysis of the flow field over a family of ogive bodies (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, 1977., 1977), also by Ronnie W. Guy, United States. Army. Missile Command, and inc Science Applications (page images at HathiTrust) Redstone Arsenal (Ala.): Theoretical analysis of the flow field over a family of ogive bodies : a supplement to MIRADCOM technical report TD-CR-77-5I (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Systems Simulation Directorate, Technology Laboratory, 1979., 1979), also by R. L. Richardson, B. Z. Jenkins, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Theoretical analysis of the flow field over a family of ogive bodies. Volume II (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Technology Laboratory, 1979., 1979), also by R. L. Richardson, B. Z. Jenkins, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Thrust effects on missile aerodynamics (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Directorate for Research, Development, Enginering and Missile Systems Laboratory, 1971., 1971), also by R. A. Deep, C. E. Brazzel, James H. Henderson, and United States. Army. Missile Command (page images at HathiTrust) Redstone Arsenal (Ala.): Transonic flow-field calculation around ogive cylinders by nonlinear-linear stretching method (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1970., 1970), also by Jain-Ming Wu, Kinya Aoyama, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Transonic flow fields around various bodies of revolution including preliminary studies on viscous effects with and without plume : summary report (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1971., 1971), also by Jain-Ming Wu, Trevor H. Moulden, Kinya Aoyama, United States. Army. Missile Command, and University of Tennessee (System). Space Institute (page images at HathiTrust) Redstone Arsenal (Ala.): Transonic wind tunnel investigation of thrust effects on the longitudinal stability characteristics of several body-fin configurations : sting-mounted model with normal-jet plume simulator (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research, Development, and Engineering Laboratory, 1974., 1974), also by James H. Henderson, Chrysler Corporation, and Development United States. Army. Missile Command. Research (page images at HathiTrust) Redstone Arsenal (Ala.): User's manual for the Martin-Marietta high angle of attack aerodynamic methodology for body tail missiles (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Directorate, Technology Laboratory, 1978., 1978), also by Gary C. Winn and United States. Army. Missile Command (page images at HathiTrust)
Find more by Redstone Arsenal (Ala.) at your library, or elsewhere.
|