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    Planetary/DoD Entry Technology Flight Experiments. Volume 2: Planetary Entry Flight Experiments

    H. E. Christensen / R. J. Krieger / W. R. Mcneilly et al. | NTIS | 1976
    of the outer planets' atmospheres was established. Disciplines of thermodynamics, orbital mechanics, aerodynamics propulsion, structures ...
    Schlagwörter: Atmospheric entry

    Numerical modeling and flight experiments of glider dynamics in non-uniform winds

    Bouskela, Adrien / Shkarayev, Sergey V. | TIBKAT | 2023

    Wind Estimation using an H∞ Filter with Fixed-Wing Aircraft Flight Test Results

    Gahan, Kenneth / Hopwood, Jeremy W. / Woolsey, Craig A. | TIBKAT | 2023

    Flight Simulator Result Comparing Three Aircraft Configurations: Quasi-Static, Flexible and Extended Flexibility

    Moreira, Fernando J. Oliveira / Drewiacki, Daniel / Junior, Marco Antonio De Oliveira Alves et al. | TIBKAT | 2023

    Space Tug Aerobraking Study. Volume 2 Technical

    C. J. Corso / C. L. Eyer | NTIS | 1972
    The feasibility and practicality of employing an aerobraking trajectory for return of the reusable Space Tug from geosynchro-nous and other ...
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics

    Generic Aerocapture Atmospheric Entry Study, Volume 1

    NTIS | 1980
    An atmospheric entry study to fine a generic aerocapture vehicle capable of missions to Mars, Saturn, and Uranus is reported. A single ...
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Atmospheric entry simulation

    Integrated Propulsion for Near-Earth Space Missions. Volume 2: Technical

    C. L. Dailey / H. F. Meissinger / R. H. Lovberg et al. | NTIS | 1981
    The calculation approach is described for parametric analysis of candidate electric propulsion systems employed in LEO to GEO missions ...
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Atmospheric density

      Integrated Propulsion for Near-Earth Space Missions. Volume 2: Technical

      C. L. Dailey / H. F. Meissinger / R. H. Lovberg et al. | NTIS | 1981
      The calculation approach is described for parametric analysis of candidate electric propulsion systems employed in LEO to GEO missions ...
      Schlagwörter: Spacecraft Trajectories & Flight Mechanics

    Study of Direct Versus Orbital Entry for MARS Missions. Volume 2 - Parametric Studies, Final Analyses, Conceptual Designs

    R. S. Wiltshire | NTIS | 1968
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Atmospheric entry

    Dynamic Stability of Deployable Aeroshells at Supersonic Speeds

    Innocenzi, Pietro / Bruce, Paul J. / Navarro-Martinez, Salvador | TIBKAT | 2023

    Conceptualization and Analysis of Various Mid-Air Launch Technique for Parasite Aircraft

    Joshi, Harshal V. / Salahudden, Salahudden / Ghosh, Ajoy K. | TIBKAT | 2023

    Six-Degree-of-Freedom Rocket Landing Optimization by Augmented Convex-Concave Decomposition

    Sagliano, Marco / Lu, Ping / Seelbinder, David et al. | TIBKAT | 2023

    Numerical Investigations of Subscale Flexible High Aspect Ratio Aircraft on a Dynamic Wind Tunnel Rig

    Navaratna, Punsara D. Banneheka / Pontillo, Alessandro / Rezgui, Djamel et al. | TIBKAT | 2023

    Reachability Analysis of a Hypersonic Glide Vehicle using Particle Swarm Optimization

    Rataczak, Jens A. / McMahon, Jay W. / Boyd, Iain D. | TIBKAT | 2023

    Customized Real-Time First-Order Methods for Onboard Dual Quaternion-based 6-DoF Powered-Descent Guidance

    Kamath, Abhinav G. / Elango, Purnanand / Kim, Taewan et al. | TIBKAT | 2023

    Nonlinear Multiplicative Smoothing Applied to Trajectory Recovery for GPS/INS-Aided Navigation

    Adams, Davis W. / Peck, Caleb / Majji, Manoranjan | TIBKAT | 2023