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Main Propellant Tank Pressurization System Study And Test Program
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Book Synopsis Main Propellant Tank Pressurization System Study and Test Program by : Lockheed-Georgia Company
Download or read book Main Propellant Tank Pressurization System Study and Test Program written by Lockheed-Georgia Company and published by . This book was released on 1961 with total page 95 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design information on liquid propellant tank pressurization systems is presented. The areas covered are: pressurization gas requirements, including hand calculation procedures and nomographs; tankage, including material properties and volume and wall area curves; and components, including stored He system weight curves and a simple but accurate heat exchanger design method.
Book Synopsis Main Propellant Tank Pressurization System Study and Test Program. Volume Iii. Design Handbook by : LOCKHEED AIRCRAFT CORP MARIETTA GA.
Download or read book Main Propellant Tank Pressurization System Study and Test Program. Volume Iii. Design Handbook written by LOCKHEED AIRCRAFT CORP MARIETTA GA. and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design information on liquid propellant tank pressurization systems is presented. The areas covered are: pressurization gas requirements, including hand calculation procedures and nomographs; tankage, including material properties and volume and wall area curves; and components, including stored He system weight curves and a simple but accurate heat exchanger design method. (Author).
Book Synopsis Main Propellant Tank Pressurization System Study and Test Program. Volume Iv. Computer Program by : LOCKHEED AIRCRAFT CORP MARIETTA GA.
Download or read book Main Propellant Tank Pressurization System Study and Test Program. Volume Iv. Computer Program written by LOCKHEED AIRCRAFT CORP MARIETTA GA. and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: A COMPUTER PROGRAM WHICH CAN BE USED TO DETERMINE THE PRESSURIZING GAS REPUIREMENTS FOR A MISSILE PROPELLANT TANK PRESSURIZATION SYSTEM IS DESCRIBED. The program is applicable to both cryogenic and storable propellants when pressurized with stored gas, evaporated propellant, and main tank injection methods of pressurization. (Author).
Book Synopsis Main Propellant Tank Pressurization System Study and Test Program by : LOCKHEED AIRCRAFT CORP MARIETTA GA.
Download or read book Main Propellant Tank Pressurization System Study and Test Program written by LOCKHEED AIRCRAFT CORP MARIETTA GA. and published by . This book was released on 1961 with total page 147 pages. Available in PDF, EPUB and Kindle. Book excerpt: A discussion is presented on the evaporated propellant (EP) and main tank injection (MTI) systems for main propellant tank pressurization. Results of testing with liquid H, liquid N, UDMH, NTO (N2O4), N2H4, 50-50 UDMH/N2H4, RP-1, BrF5, ClF3 and B5H9 are presented. The MTI method of tank pressurization is believed feasible for the following combinations: NTO into UDMH; NTO into 50-50 UDMH/N2H4; UDMH into NTO; 50-50 UDMH/N2H4 into NTO; N2H4 into NTO; ClF3 into B5H9. The EP method appears practical for liquid H, liquid O and NTO, while the MTI method appears practical for the combination NTO and 50-50 UDMH/N2H4, and NTO and UDMH in either the fuel or oxidizer tank.
Book Synopsis Pressurization Systems Design Guide: pt.A-B. Design procedures and data by : Aerojet-General Corporation
Download or read book Pressurization Systems Design Guide: pt.A-B. Design procedures and data written by Aerojet-General Corporation and published by . This book was released on 1966 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressurization Systems Design Guide: System analysis and selection by : Aerojet-General Corporation
Download or read book Pressurization Systems Design Guide: System analysis and selection written by Aerojet-General Corporation and published by . This book was released on 1966 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis of Cryogenic Propellant Tank Pressurization Based Upon Experiments and Numerical Simulations by : Carina Ludwig
Download or read book Analysis of Cryogenic Propellant Tank Pressurization Based Upon Experiments and Numerical Simulations written by Carina Ludwig and published by . This book was released on 2014-09-04 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt: Focus of this study is the pressurization system of a cryogenic liquid propellant tank for the launcher application. Objective of the pressurization system is to provide the required pressure evolution in the propellant tank for a proper operation of the engine. The motivation of this study is an improved understanding of the complex fluid-dynamic and thermodynamic phenomena during the active-pressurization process of cryogenic propellants in order to optimize the on-board pressurant gas mass. Therefore ground experiments, numerical simulations and analytical considerations were performed for the investigation of the initial active-pressurization phase. For the performed experiments, liquid nitrogen was used as cryogenic model propellant, which was actively pressurized under normal gravity conditions up to different final tank pressures. As pressurant gases, gaseous nitrogen and gaseous helium were used with different inlet temperatures. For the numerical analyses the commercial CFD program Flow-3D, a three-dimensional Navier-Stokes equation solver, was used.
Download or read book Proceedings written by and published by . This book was released on 1962 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Propellant Tank Pressurization Requirements by Dimensional Analysis by : J. F. Thompson
Download or read book Prediction of Propellant Tank Pressurization Requirements by Dimensional Analysis written by J. F. Thompson and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of the NASA-University Conference on the Science and Technology of Space Exploration by :
Download or read book Proceedings of the NASA-University Conference on the Science and Technology of Space Exploration written by and published by . This book was released on 1962 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: A Chinese boy's greatest wish is to be an artist but he is too poor to buy a good brush until a wizard appears and gives him one with magic powers.
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 2180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1966 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pressurization Systems Design Guide by : Aerojet-General Corporation
Download or read book Pressurization Systems Design Guide written by Aerojet-General Corporation and published by . This book was released on 1966 with total page 462 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Chemical Rocket Propulsion written by and published by . This book was released on 1962 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Development and Demonstration of Main Tank Injection (mti) Pressurization System by : R. J. Kenny
Download or read book Development and Demonstration of Main Tank Injection (mti) Pressurization System written by R. J. Kenny and published by . This book was released on 1963 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt: A liquid rocket engine main tank injection (MTI) pressurization system which employs a chemical method of propellant tank pressurization, is studied. The process is initiated by injecting a small quantity of hypergolic reagent into the main propellant tank. The technical approach has been to study the important factors influencing the pressurization process by laboratory experiments and analytically determine system operating characteristics to evaluate various possible designs. Several engineering studies were completed initially to establish the pertinent design requirements of such a system, identify desirable configurations, and determine the most promising applications. Verification of the theoretical performance and development of a practical system was accomplished by a considerable amount of testing on 5 1/3-cu ft thick wall spherical tanks and subsequent demonstration in a 2,000-gal. full-scale flight-type ground test article. The research fixture was fabricated to investigate the actual reaction process and de develop components and operating procedures on a small-scale basis at pressures up to 200 psia.
Book Synopsis Proceedings of the NASA-University Conference on the Science and Technology of Space Exploration, Chicago, Illinois, November 1-3, 1962 by : United States. National Aeronautics and Space Administration
Download or read book Proceedings of the NASA-University Conference on the Science and Technology of Space Exploration, Chicago, Illinois, November 1-3, 1962 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 992 pages. Available in PDF, EPUB and Kindle. Book excerpt: