Optimal payload trajectory characteristics for winged booster vehicles
Optimal payload trajectory characteristics for winged booster vehicles
Elliott, J. R.↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A Fourier transform technique for the prediction of torsional transients for a spacecraft from flight data of another spacecraft using the same booster
Fourier transform for predicting torsional transients for one spacecraft based on flight data of another with same booster
Trubert, M. R.↗
Dynamic stability of space vehicles. Volume 14 - Testing for booster propellant sloshing parameters
Recommended procedures for stability, control, and structural loading analysis of large liquid fueled rocket booster sloshing parameters
Eggleston, D. M.↗
An optical fixed control structure design with minimal sensitivity for a large elastic booster
Optimal fixed control structure design with minimal sensitivity for large elastic booster
Dangelo, H.↗
Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight
Thrust vector deflection stability analysis for minimum control requirements of booster vehicles during atmospheric flight
Borsody, J.↗
OGO-E space vehicle response to transient loading at Atlas booster engine cutoff
Computer program for OGO-E vehicle response analysis to transient loading during Atlas booster burnout
Alper, M. E.↗
Booster and spacecraft electrostatic phenomena - Causes, effects, and prevention
Booster and spacecraft electrostatic phenomena /causes, effects, and prevention/
Coleman, W.↗
A study of fully manual and augmented manual control systems for the Saturn 5 booster using analytical pilot models
Fully-manual and augmented-manual control systems for Saturn 5 booster studied by emperically based mathematical models for pilot
Jex, H. R.↗
Rapid determination of near-optimum linear pitch programs for rocket boosters.
Linear segment pitch rate program for near optimum trajectory for rocket boosters
Rosenbaum, R.↗
Evaluation of concepts for reuse of large booster nozzles.
Large booster nozzle reuse, discussing design, refurbishment, performance, costs and test evaluation
Bailey, R. L.↗
Orbiting astronomical observatory A-2 space vehicle response to transient loadings at Atlas booster engine cutoff
Predicting structural response of OAO A-2 to transient loading at Atlas booster engine cut-off
Garba, J. A.↗
Experimental bending strength of an Atlas LV-3C booster beyond compressive skin wrinkling
Tests of bending strength on full scale model of Atlas LV-3C booster
Miller, R. P.↗
Evaluation of a pilot describing function method applied to the manual control analysis of a large flexible booster
Evaluation of pilot describing function method applied to manual control analysis of large flexible booster in Saturn 5 launch vehicle simulator
Creer, B. Y.↗
Analysis of Saturn booster performance by conventional control theory techniques Volume 1 of final report, 4 May 1967 - 3 Nov. 1968
Analysis of Saturn booster flight control system stability by linear feedback theory with emphasis on root locus technique
Smith, E. J.↗
Evaluation of concepts for reuse of large booster nozzles.
Large booster nozzle reuse, discussing design, refurbishment, performance, costs and test evaluation
Bailey, R. L.↗
Space shuttle booster return performance
Space shuttle booster entry and subsonic performance analysis
Bithell, R. A.↗
Recoverable single stage spacecraft booster Patent
Recoverable, reusable single stage booster capable of injecting large payloads into circular earth orbit
Bono, P.↗
Low-subsonic longitudinal aerodynamic characteristics of a twin-body space-shuttle booster configuration
Low subsonic longitudinal aerodynamic characteristics of twin body space shuttle booster configuration using low turbulence pressure tunnel - graphs
Spencer, B., Jr.↗