Synonyme wurden verwendet für: Cluster design flight
Suche ohne Synonyme: keywords:(Cluster flight orbit design)

1–20 von 63 Ergebnissen
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    Trajectory Design Considerations for Lunar Surface to Near Rectilinear Halo Orbit Rendezvous

    C. W. Foster / P. M. Brandt / M. M. Pellegrino et al. | NTIS | 2023
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Mission design , Near rectilinear halo orbit

    Trajectory Design Considerations for Low Lunar Orbit to Near Rectilinear Halo Orbit Transfers

    C. W. Foster / P. M. Brandt / M. M. Pellegrino | NTIS | 2022
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Mission design , Near rectilinear halo orbit

    Orbital Debris Shape Characterization Project Abstract

    J. Pease | NTIS | 2016
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Orbit determination , Computer aided design

    X-33 and RLV for the Future

    J. D. Bland | NTIS | 2000
    Schlagwörter: Single stage to orbit vehicles , Functional design specifications , Flight tests

    Six Degree of Freedom Simulation System for Evaluating Automated Rendezvous and Docking Spacecraft

    K. H. Rourke / R. K. Tsugawa | NTIS | 1991
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Flight simulation , Orbit transfer vehicles , Flight simulators , Automatic flight control , Spacecraft design

    Semi-Major Axis Knowledge and GPS Orbit Determination

    J. R. Carpenter / E. R. Schiesser | NTIS | 2000
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Orbit determination , Spacecraft design , Flight characteristics

    Preparing GMAT for Operational Maneuver Planning of the Advanced Composition Explorer (ACE)

    R. H. Qureshi / S. P. Hughes | NTIS | 2014
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Design analysis , Orbit determination

    Technology Requirements for Advanced Earth Orbital Transportation Systems. Volume 2: Summary Report

    A. K. Hepler / E. L. Bangsund | NTIS | 1978
    Schlagwörter: Single stage to orbit vehicles , Horizontal flight , Structural design

    Engineering Study and Experiment Definition for an APOLLO Applications Program Experiment on Vehicle Disturbances Due to Crew Activity

    C. H. Murrish / J. R. Tewell | NTIS | 1967
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Experiment design , Design , Flight , Orbit

    Overview of the Altair Lunar Lander Thermal Control System Design

    R. A. Stephan | NTIS | 2010
    Schlagwörter: Control systems design , Manned space flight , Orbit insertion

    Requirements, Design and Prototype of a Virtual User Interface for the AFIT Virtual Spaceplane

    J. M. Lewis | NTIS | 1997
    Schlagwörter: Flight simulators , Computer aided design , Low orbit trajectories , Design criteria , Space flight , Aircraft design

    1999 Flight Mechanics Symposium

    NTIS | 1999
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Flight mechanics , Control systems design , Orbit determination , Orbit decay

    Applications Study of AERO-Maneuvering Orbit-to-Orbit Shuttle (Amoos), Executive Summary

    J. White | NTIS | 1976
    Schlagwörter: Design analysis , Orbit maneuvering engine (Space shuttle) , Flight tests

    Monte Carlo Analysis as a Trajectory Design Driver for the Transiting Exoplanet Survey Satellite (TESS) Mission

    C. Nickel / J. Parker / D. Dichmann et al. | NTIS | 2016
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Orbit determination , Design analysis

    Orl Experiment Program. Volume C - Guidelines for Comprehensive Flight Program

    NTIS | 1966
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Experiment design , Flight , Orbit

    Applications Study of AERO-Maneuvering Orbit-to-Orbit Shuttle (AMOOS)

    J. White | NTIS | 1976
    Schlagwörter: Design analysis , Orbit maneuvering engine (Space shuttle) , Flight tests

    Mercator: A New Ground System for Orbit and Attitude Control

    B. Belon / J. C. Berges / G. Campan et al. | NTIS | 1986
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Control systems design , Orbit calculation

    Matlab as a Robust Control Design Tool

    I. M. Gregory | NTIS | 1994
    Schlagwörter: Spacecraft Trajectories & Flight Mechanics , Control systems design , Design analysis , Flight control , Single stage to orbit vehicles