Last edited by Disar
Tuesday, July 28, 2020 | History

2 edition of System technology analysis of aeroassisted orbital transfer vehicles. found in the catalog.

System technology analysis of aeroassisted orbital transfer vehicles.

System technology analysis of aeroassisted orbital transfer vehicles.

moderate lift/drag (0.75-1.5) : phase II final report.

  • 356 Want to read
  • 31 Currently reading

Published by Re-entry Systems Operations, General Electric in Philadelphia, PA .
Written in English

    Subjects:
  • Orbital transfer (Space flight),
  • Space flight.

  • Edition Notes

    SeriesNASA-CR -- 179142., NASA contractor report -- NASA CR-179142.
    ContributionsGeneral Electric Company. Re-entry Systems Operations., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17660383M

    The OTV figured in the 'Pioneering the Space Frontier' policy report. These vehicles would transport crews and equipment from space stations in low Earth orbit to lunar orbit. The Orbital Transfer Vehicle concept was renamed by NASA the Lunar Transfer Vehicle in to stress its importance for manned lunar base missions. University of Cincinnati Libraries. PO Box Cincinnati, Ohio Phone: Contact Us | Staff DirectoryAuthor: Ted Baldwin.

    ASTV - Aeroassisted Space Transfer Vehicles. Looking for abbreviations of ASTV? Aero-Space Technology Advisory Committee; Aero-Tropics Air Services; Aeroacrophobia; aeroallergen; aeroallergen; aeroallergen; Aeroambulance; Aeroambulance; Aeroassist Flight Experiment; Aeroassisted Orbital Transfer Vehicle; Aeroassisted Space Transfer. a transfer orbit by the failure of its apogee motor. A companion paper looks at a variety of specific missions, suggested originally by this tradespace analysis, that concentrate on servicing groups of satellites in similar orbits. MATE METHOD In MATE, user needs are defined in terms of the system’s attributes, or capabilities of the desiredFile Size: 1MB.

    Aironet System Tray Utility (Cisco) Allentown Secure Treatment Unit (Pennsylvania) Altai State Technical University (Barnaul, Russia) Anti-Stock Theft Unit; Archangelsk State Technical University (Russia) Astrakhan State Technical University (Russia) Anthony Saves the World (online video series) ASEAN Science and Technology Week. The basics of aerothermodynamics are treated in this book with special regard to the fact that outer surfaces of hypersonic vehicles primarily are radiation cooled. The implications of this fact are different for different vehicle classes. In any case the properties of both attached viscous and separated flows are of importance in this regard.


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System technology analysis of aeroassisted orbital transfer vehicles Download PDF EPUB FB2

The item System technology analysis of aeroassisted orbital transfer vehicles: moderate lift/drag (): phase I final report, Volume IB, Part I, Study results represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Indiana State Library.

Get this from a library. System technology analysis of aeroassisted orbital transfer vehicles. Volume IA, Part 1, Executive summary: moderate lift/drag (): phase I final report. [United States.

National Aeronautics and Space Administration.;]. This final report of the "System Technology Analysis of Aeroassisted Orbital Transfer Vehiclps: Moderate Lift/Drag ()" was prepared by the General Electric Company, Space Systems Division for the National Aeronautics and Space Administration's George C.

Marshall Space Flight Center (MSFC) in accordance with Contract NAS Get this from a library. System technology analysis of aeroassisted orbital transfer vehicles. Volume II, Supporting research and technology report: moderate lift/drag (): phase I & II final report. [General Electric Company.

Re-entry Systems Operations.; United States. National Aeronautics and Space Administration.;]. Dickman, G. Orbital Transfer Vehicle Concept Definition and Systems Analysis Study - Volume 2: OTV Concept Definition and Evaluation. Book 3: Subsystem Trade Studies, Boeing Aerospace Company, NASA Contract NAS, NASA-CR, Rev.

1, July Cited by: 1. orbital transfer vehicle concept definition and system analysis study final report cchcept (basa-cb- depiniiticn ) orbital anc syszeb 16abseeb ahalysis vehicle study. vcluplfi id: executive suhbdey. phase 2 final refort (general dynamics corp.) 55 p unclas b 10 18 cscl 22b g3/18 volume ia executive summary phase 2File Size: 2MB.

Minimum-Fuel Low-Earth-Orbit Aeroassisted Orbital Transfer of Small Spacecraft Article in Journal of Spacecraft and Rockets 48(4) July.

Full text of "Orbital transfer vehicle concept definition and system analysis study, Volume 1-A: Executive summary supplement" See other formats J ^ MCR NAS Volume l-A Executive Summary Supplement Orbital Transfer Vehicle Concept Definition And System Analysis Study (NASI-Cfi-lSSS'i^) CBfillAL IfiAK£l£B VEHICLE CCIiCECI DEFINIIlCt AhC.

American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Full text of "Orbital transfer vehicle concept definition and systems analysis study, volume 4" See other formats 4 ORBITAL TRANSFER VEHICLE CONCEPT DEFINITION AND SYSTEMS ANALYSIS STUDY FINAL REPORT -PHASE I VOLUME IV SPACE STATION ACCOMMODATIONS NASA/MSFC [^^gQ_2g^ i!*^*"^^~''Voi-4) ORBITAL.

More recently, optimal aeroassisted orbital transfer has been considered for vehicles subject to high heating rate constraints [4, 5, 6, 7]. In addition, multiple. of small spacecraft aeroassisted orbital transfer. One particular study of small spacecraft aeroassisted orbital transfer is the work of Ref.

Specifically, Ref. 20 considers the problem of minimum-fuel heating rate-constrained aeroassisted orbital transfer under the assumption of impulsive thrust.

This paper reviews optimal trajectories for aeroassisted orbital transfer (AOT). The basic idea is to combine space maneuvers and atmospheric maneuvers so as to achieve propellant savings vis-avis purely propulsive maneuvers.

For the atmospheric pass, both angle of attack control and angle of bank control are : A. Miele, B. Lee. The objectives of the Orbital Transfer Vehicle (OTV) Concept Definition and Systems Analysis study, conducted by General Dynamics Space Systems Division under company funds with data provided to NASA-MSFC, were to define the requirements, concepts, and evolutionary approaches for development of an OTV for reusable operations to GEO and beyond, including Cited by: 1.

The concept of aeroassisting for orbital transfer has been recognized as one of the critical technologies for pioneering the space frontier. In space transportation systems, aeroassisting (or aerobraking), defined as the deceleration resulting from the effects of atmospheric drag upon a vehicle during orbital operations, opens new mission opportunities, especially with regard to Cited by: In spaceflight, an orbital maneuver (otherwise known as a burn) is the use of propulsion systems to change the orbit of a spacecraft far from Earth (for example those in orbits around the Sun) an orbital maneuver is called a deep-space maneuver (DSM).

[not verified in body]The rest of the flight, especially in a transfer orbit, is called coasting. Bérend, S. Bertrand and C. Jolly, “Optimization Method for Mission Analysis of Aeroassisted Orbital Transfer Vehicles”, in Aerospace Science and Technology, vol.

11, pp.Book. University of Cincinnati Libraries. PO Box Cincinnati, Ohio Phone: Contact Us | Staff Directory. Orbital transfer vehicle concept definition and system analysis study (SuDoc NAS ) [James H.

Nelson] on *FREE* shipping on qualifying : James H. Nelson. pulsive orbital transfer, the problems investigated have covered the full range, from high-thrust to low-thrust propulsivc systems, from the simple Hohmann transfer to the complex multi-impulse rendezvous problem, it is expected that in the coming years thc analysis of aeroassisted orbit transfer will become more and more involved.

The other is the emergence and maturing of the discrete numerical methods of aerodyn- ics/aerothermodynamics complementary to the ground-simulation facilities, with the parallel enormous growth of computer power.

Airbreathing hypersonic flight vehicles are, in contrast to aeroassisted re-entry vehicles, drag sensitive. Chapter in a book in a series Sutton, K., "Air Radiation Revisited," Thermal Design of Aeroassisted Orbital Transfer Vehicles, edited by H. F. Nelson, Vol.

96, Progress in Astronautics and Aeronautics, AIAA, New York,pp. Conference paper.The system analyzed is a unstable first order plant, driven by a Bang-Bang actuator, stabilized by a nonlinear adaptive perturbation filter.

A describing function model of the actuator is used in this analysis. This system is implemented on a digital computer, and in analog circuit form, to demonstrate the practicality of the method.