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Author : J. P. McDonald
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Propellant Feed Sub-system for the X-34 Main Propulsion System written by J. P. McDonald and published by . This book was released on 1998 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : T. M. Brown
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Propellant Management and Conditioning Within the X-34 Main Propulsion System written by T. M. Brown and published by . This book was released on 1998 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : C. E. Vaughan
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Propellant Feed Subsystem for a 26kW Flight Arcjet Propulsion System written by C. E. Vaughan and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 314 pages
Book Rating : 4.:/5 (227 download)
Download or read book Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume II -- Propulsion Stage System Design written by ROCKETDYNE CANOGA PARK CALIF. and published by . This book was released on 1970 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume provides the details of the selected propellant feed system design. The recommended configuration, consisting of a 1.41 ellipsoidal oxidizer tank, a 1.41 ellipsoidal fuel tank with a short cylindrical section and a conical/cylindrical shell has a mass fraction of 0.854, a dry weight of 2028 lb and a delta V capability of 20,197 to 21,765 ft/sec (with a 2000 lb payload) which varied over this range depending on the duty cycle and thrust level used. With prior knowledge of the duty cycle to be performed, i.e. if the mission is known after achieving orbit, the delta V capability rises to 22,800 ft/sec with the same payload weight. Extended mission capability to 180 days is also presented. A summary of the design, assembly plans, performance data and reliability data are given followed by design details, structural analyses and manufacturing plans for each selected vehicle subsystem.
Author : R. H. Champion
Publisher :
ISBN 13 :
Total Pages : 19 pages
Book Rating : 4.:/5 (472 download)
Download or read book X-34 Main Propulsion System Design and Operation written by R. H. Champion and published by . This book was released on 1998 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : DP Mishra
Publisher : CRC Press
ISBN 13 : 1351708414
Total Pages : 364 pages
Book Rating : 4.3/5 (517 download)
Download or read book Fundamentals of Rocket Propulsion written by DP Mishra and published by CRC Press. This book was released on 2017-07-20 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Author :
Publisher :
ISBN 13 :
Total Pages : 109 pages
Book Rating : 4.:/5 (227 download)
Download or read book STORABILITY DEMONSTRATION PROPELLANT FEED SYSTEMS. written by and published by . This book was released on 1967 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the design, fabrication, testing, and delivery of Storable Prepackaged Propellant Systems (SPPS) for subsequent use in a storability investigation, by the Air Force Rocket Propulsion Laboratory (AFRPL), of a liquid rocket propellant feed system. Each of the twenty-three delivered systems consists of a 15 gallon propellant tank which contains either a Surface Force Orientation (SFO) device, or a Rolling Diaphragm (RD) positive expulsion device, along with one of three different pressurization subsystems. The subsystems include a Liquid Propellant Gas Generator (LPGG), a Solid Propellant Gas Generator (SPGG), or a Stored Gas Device (SGD). The systems were delivered to AFRPL, hermetically sealed, with their respective propellants; Mixed Hydrazine Fuel (MHF-5), Nitrogen Tetroxide (N2O4), or a third propellant; loaded in the propellant tanks.
Author :
Publisher :
ISBN 13 :
Total Pages : 616 pages
Book Rating : 4.F/5 ( download)
Download or read book Aerospace America written by and published by . This book was released on 2006 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 338 pages
Book Rating : 4.:/5 (227 download)
Download or read book Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume III--Part A - Screening and Optimization Analyses written by ROCKETDYNE CANOGA PARK CALIF. and published by . This book was released on 1970 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt: Part A of this volume provides: the study ground rules and vehicle environments to which the propellant feed system is designed; a Configuration Optimization Study that allowed selection of the propellant tanks and shell; an impact study of an integrated attitude control system (F2/H2) as compared to the reference Compound A/MHF-5 attitude control system; and screening and optimization analyses that led to the design requirements for the external load-carrying shell, engine thrust structure, thermal control coating, engine actuators, tank support struts, insulation systems, ground hold vent-free oxidizer tank system and flight tank-pressure-control system.
Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 539 pages
Book Rating : 4.:/5 (227 download)
Download or read book Advanced Maneuvering Propulsion System (Convair Propellant Feed System Design). Volume III--Optimization Studies written by ROCKETDYNE CANOGA PARK CALIF. and published by . This book was released on 1970 with total page 539 pages. Available in PDF, EPUB and Kindle. Book excerpt: The optimum propellant tank shapes were found to be a spherical LH2 tank and in a LF2 tank with bulkhead ratio of 1.2. Both tanks are constructed of aluminum. Tank mounted super-insulation affords slightly better performance than shroud mounted insulation. Screen start baskets were selected as superior to dielectrophoretic devices and positive expulsion devices for use in orienting the propellants during coast. Capacitance probes were selected as the propellant management mass sensors due to their superior accuracy and proven reliability. The selected pressurization system utilizes a pressurant 'bubble-up' concept, where the pressurizing medium, helium, is bubbled through the propellants during the pressurizing cycle. The results of these optimization studies were used as the basis of the selected configuration design described in Volume II.
Author :
Publisher :
ISBN 13 :
Total Pages : 1044 pages
Book Rating : 4.F/5 ( download)
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 1044 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 659 pages
Book Rating : 4.:/5 (227 download)
Download or read book Advanced Maneuvering Propulsion System (Convair Propellant Feed System Design). Volume II - Selected Configuration Description written by ROCKETDYNE CANOGA PARK CALIF. and published by . This book was released on 1970 with total page 659 pages. Available in PDF, EPUB and Kindle. Book excerpt: The optimized design consists of aluminum propellant tanks, a cylindrical outer structural shell, tank mounted multi-layer insulation, a propellant management system with capacitance probe propellant mass sensors, and screen start baskets to provide propellants at the tank outlets during zero g coast. A pressurization system is used which keeps the propellant tank constituents in thermal equilibrium at all times, thereby maintaining a constant state of readiness. The propellant inlet ducts are designed to maintain liquid propellants in near proximity to the engine inlet, providing an instant start capability.
Author : Hans-P. Berg
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Propellant Storage and Feed System for the Radiofrequency Ion Propulsion System RITA written by Hans-P. Berg and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 728 pages
Book Rating : 4.:/5 (3 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 728 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Dieter K. Huzel
Publisher : AIAA
ISBN 13 : 9781600864001
Total Pages : 452 pages
Book Rating : 4.8/5 (64 download)
Download or read book Modern Engineering for Design of Liquid-Propellant Rocket Engines written by Dieter K. Huzel and published by AIAA. This book was released on 1992 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 556 pages
Book Rating : 4.0/5 ( download)
Download or read book 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 11-14, 2004, Fort Lauderdale, FL.: 04-3850 - 04-3899 written by and published by . This book was released on 2004 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Research Council
Publisher : National Academies Press
ISBN 13 : 0309266564
Total Pages : 115 pages
Book Rating : 4.3/5 (92 download)
Download or read book Reusable Booster System written by National Research Council and published by National Academies Press. This book was released on 2013-01-10 with total page 115 pages. Available in PDF, EPUB and Kindle. Book excerpt: On June 15, 2011, the Air Force Space Command established a new vision, mission, and set of goals to ensure continued U.S. dominance in space and cyberspace mission areas. Subsequently, and in coordination with the Air Force Research Laboratory, the Space and Missile Systems Center, and the 14th and 24th Air Forces, the Air Force Space Command identified four long-term science and technology (S&T) challenges critical to meeting these goals. One of these challenges is to provide full-spectrum launch capability at dramatically lower cost, and a reusable booster system (RBS) has been proposed as an approach to meet this challenge. The Air Force Space Command asked the Aeronautics and Space Engineering Board of the National Research Council to conduct an independent review and assessment of the RBS concept prior to considering a continuation of RBS-related activities within the Air Force Research Laboratory portfolio and before initiating a more extensive RBS development program. The committee for the Reusable Booster System: Review and Assessment was formed in response to that request and charged with reviewing and assessing the criteria and assumptions used in the current RBS plans, the cost model methodologies used to fame [frame?] the RBS business case, and the technical maturity and development plans of key elements critical to RBS implementation. The committee consisted of experts not connected with current RBS activities who have significant expertise in launch vehicle design and operation, research and technology development and implementation, space system operations, and cost analysis. The committee solicited and received input on the Air Force launch requirements, the baseline RBS concept, cost models and assessment, and technology readiness. The committee also received input from industry associated with RBS concept, industry independent of the RBS concept, and propulsion system providers which is summarized in Reusable Booster System: Review and Assessment.
