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Sunday, July 26, 2020 | History

3 edition of Design and performance analysis of an aeromaneuvering orbital-transfer vehicle concept found in the catalog.

Design and performance analysis of an aeromaneuvering orbital-transfer vehicle concept

Design and performance analysis of an aeromaneuvering orbital-transfer vehicle concept

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Published by National Aeronautics and Space Administration, Ames Research Center, For sale by the National Technical Information Service in Moffett Field, Calif, [Springfield, Va .
Written in English

    Subjects:
  • Space vehicles -- Attitude control systems.,
  • Reusable space vehicles.

  • Edition Notes

    StatementGene P. Menees.
    SeriesNASA technical memorandum -- 86848.
    ContributionsAmes Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15285009M

      involve off-mission design performance, flight performance analysis, and general component performance mapping. For analysis tasks, the design can come from a sizing task, from a previous NDARC job, or an independent design database. The culmination of this paper is an aircraft NDARC input set where the geometry and aerodynamics stem from the. The conceptual design was constructed and successfully tested. Further aerodynamic analysis for the full configuration was carried out to evaluate the performance during the flight envelope. The findings of this analysis could be utilized to further improve the aerodynamics of the existing design, and enhance stability and performance.

    analysis and design techniques became available. Several flight technology 52 Aeroconfigured Orbital Transfer Vehicles 82 53 Configuration Design Trend 84 54 Advanced Manned Interceptor Test 86 55 Hypersonic Airbreathing Cruise Vehicles 87 AOTV Aeromaneuvering Oribtal Transfer Vehicle. : Analysis and Design of Flight Vehicle Structures () by Bruhn, E. F. and a great selection of similar New, Used and Collectible Books available now at great prices.

    @article{osti_, title = {Particle bed reactor propulsion vehicle performance and characteristics as an orbital transfer rocket}, author = {Horn, F L and Powell, J R and Lazareth, O W}, abstractNote = {The particle bed reactor designed for to MW power output using hydrogen as a coolant is capable of specific impulses up to seconds as a nuclear rocket. ELECTRIC ORBITAL TRANSFER VEHICLE CONCEPT EOTV Sizing Assumptions EOTV Sizing Approach EOTV Sizing Logic • EOTV Weight/Performance Summary ELECTRIC ORBITAL TRANSFER VEHICLE TRADE STUDIES Solar Array Voltage, Grid Temperature, Numbers of Thrusters


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Design and performance analysis of an aeromaneuvering orbital-transfer vehicle concept Download PDF EPUB FB2

Description. The present volume is devoted to the thermophysics of aeroassisted orbital transfer vehicle (AOTVs). As its title suggests, it is truly a progress volume for it illustrates the recent advances and current thinking with regard to AOTVs. Get this from a library.

Design and performance analysis of an aeromaneuvering orbital-transfer vehicle concept. [Gene P Menees; Ames Research Center.].

Design and performance analysis of a conical-aerobrake, orbital-transfer vehicle concept. Aerothermodynamic heating analysis of aerobraking and aeromaneuvering orbital-transfer vehicles. Systems requirements for design-optimized, lateral-turn performance were determined for reusable, space-based applications and low-earth orbits involving large multiple plane-inclination changes.

The aerothermodynamic analysis is the most advanced available for rarefied-hypersonic flow over lifting surfaces at incidence. The effects of leading-edge bluntness, low-density viscous Cited by: 3. Design and performance analysis of an aeromaneuvering orbital-transfer vehicle concept.

By G. Menees. Abstract. Systems requirements for design-optimized, lateral-turn performance were determined for reusable, space-based applications and low-earth orbits involving large multiple plane-inclination changes.

The aerothermodynamic analysis is Author: G. Menees. Aero-assisted orbital transfer vehicles are analyzed. The aerodynamic characteristics over the flight profile and three- and six-degree-of-freedom performance analyses were determined.

Menees, G. P.: Design and Performance Analysis of an Aeromaneuvering Orbital-Transfer Vehicle Concept. IAF PaperPark, C.: Calculation TJ new concept of the Preschool Quality Education Engineering the daily learning book of: new happy learning young children (. 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 TRANSFER ila ViiHiCLE CONCEPT DEFINITION AND SYSTEMS ANALYSIS.

The Orbital Transfer Vehicle (OTV) Concept Definition and System Analysis Study was conducted by General Dynamics Space System Division (GDSS), a company-funded effort under the direction of NASA/Harshall Space Flight Center (MSFC).

This study was conducted in two parts. Volume I. This report, Vol IA, summarizes the Phase 2 results. The flight strategy for a general low-earth orbit plane-change is analyzed for a conceptual, high-lift, aeromaneuvering-orbital-transfer vehicle, and applied to the important case of the 45 deg.

ORBITAL TRANSFER VEHICLE CONCEPT DEFINITION AND SYSTEM ANALYSIS STUDY VOLUME II ON CONCEPT DEFINITION AND EVALUATION BOOK 2 OTV CONCEPT DEFINITION October Rev 1 - July Prepared By: Glen J. ‘Dickman Cryogenics Manager Approved By: Initial Phase MARTIN MARIETTA ASTRONAUTICS GROUP P.O.

BOX DENVER, COLORADO   Performance Evaluation of the Atmospheric Phase of Two Aeromaneuvering Orbital Transfer Vehicles. In: Thermal Design of Aeroassisted Orbit Transfer Vehicles (H.F.

Nelson, Ed.), AIAA Progress in A&A Series, Vol. 14 U> L5 3ut -- 1st pass *^ * 2nd pass 3rd pass ** Rao, S.S. 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 SYSIEB AbAiXSIS £iuuy.

Orbit Transfer Systems with Emphasis on Shuttle Applications -NASA Technical Memorandum TMX, NASA/MSFC, April 2. Orbit Transfer Vehicle Engine Study, Phase A and Extension, Contract NASNASA/MSFC.

Orbital Transfer Vehicle (OTV) Advanced Expander Cycle Engine Point Design Study, Contract NASNASA/MSFC. Thermal Protection""; ""Thermal Protection Requirements for Near-Earth Aeroassisted Orbital Transfer Vehicle Missions""; ""Design and Performance Analysis of a Conical Aerobrake Orbital Transfer Vehicle Concept"" ""An AOTV Aeroheating and Thermal Protection Study""""Aerothermodynamic Heating Analysis of Aerobraking and Aeromaneuvering Orbital.

Talay, T. A., White, N. H., Naftel, J. Impact of Atmospheric Uncertainties and Viscous Interaction Effects on the Performance of Aeroassisted Orbital Transfer Vehicles. Thermal Design of Aeroassisted Orbital Transfer Vehicle--Progress in Astronautics and. The book begins with two introductory chapters that address fundamental principles of aerodynamics and flight stability and form a knowledge base for the student of Aerospace Engineering.

The book then covers aerodynamics of fixed wing, rotary wing and hybrid unmanned aircraft, before introducing aspects of aircraft flight stability and control. Aeronautical Engineering Ebooks. Download free Aeronautical Engineerng Books. Click on book name download.

Available in PDF. Analysis And Design Of Flight Vehicles Structures. Navigation and Guidance of Orbital Transfer Vehicle Xuefeng Li, Chaobing Li (auth.) This book uses the entire flying process, starting from ground launching of the orbital transfer vehicle (OTV) to injecting payload into earth synchronous orbit, as an example for real-world engineering practices.

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 the.

The analysis of a generic electromagnetic structure consists in the study of the distribution of the electromagnetic fields that develop inside the structure studied and particularly so in the region of the air gap.

Usually one of the first steps to be taken in the design of rotating electrical machine, is the geometric design in a CAD. This paper reports on the feasibility and cost-effectiveness of expendable and reusable orbital transfer vehicle concepts utilizing innovative low thrust, high specific impulse electric and thermal propulsion technologies.

Comparisons are made to .Prof. Newman, Page 1 Aircraft Performance Prof. Dava Newman Sr. Lecturer Pete Young Introduction to Aerospace & Design 12 February