Advanced Maneuvering Propulsion System Lockheed Propellant Feed System Design Volume Iii Part A Screening And Optimization Analyses

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Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume III--Part A - Screening and Optimization Analyses

Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 338 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume III--Part A - Screening and Optimization Analyses by : ROCKETDYNE CANOGA PARK CALIF.

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.

Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume II -- Propulsion Stage System Design

Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 314 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume II -- Propulsion Stage System Design by : ROCKETDYNE CANOGA PARK CALIF.

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.

Advanced Maneuvering Propulsion System (Convair Propellant Feed System Design). Volume III--Optimization Studies

Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 539 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Maneuvering Propulsion System (Convair Propellant Feed System Design). Volume III--Optimization Studies by : ROCKETDYNE CANOGA PARK CALIF.

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.

Notices of Changes in Classification, Distribution and Availability

Author :
Publisher :
ISBN 13 :
Total Pages : 436 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Notices of Changes in Classification, Distribution and Availability by :

Download or read book Notices of Changes in Classification, Distribution and Availability written by and published by . This book was released on 1977 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume I--Summary

Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 145 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume I--Summary by : ROCKETDYNE CANOGA PARK CALIF.

Download or read book Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume I--Summary written by ROCKETDYNE CANOGA PARK CALIF. and published by . This book was released on 1970 with total page 145 pages. Available in PDF, EPUB and Kindle. Book excerpt: A high performance LF2/LH2 maneuvering propulsion system has been defined, which provides an in orbit delta V capability in excess of 21,000 ft/sec with a 2000 pound payload. The system, which is designed for launch into a 100 nautical mile polar orbit with the Titan IIID, weighs 18,000 pounds fully loaded, has instant response and multi-start capability, while providing a nominal space residence duration of 14 days. Longer orbital stay times (up to 180 days) can be accommodated with some design modification without significantly degrading performance. This design can be used as the basis of a ground test article to demonstrate the feasibility of technical concepts applicable to a wide range of high performance stage sizes. (Author).

Advanced Maneuvering Propulsion System (Convair Propellant Feed System Design). Volume II - Selected Configuration Description

Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 659 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Maneuvering Propulsion System (Convair Propellant Feed System Design). Volume II - Selected Configuration Description by : ROCKETDYNE CANOGA PARK CALIF.

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.

Advanced Maneuvering Propulsion Technology Program

Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Maneuvering Propulsion Technology Program by : ROCKETDYNE CANOGA PARK CALIF.

Download or read book Advanced Maneuvering Propulsion Technology Program written by ROCKETDYNE CANOGA PARK CALIF. and published by . This book was released on 1970 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt: The engine design and analysis task was continued with completion of the secondary engine performance analysis, effort toward selecting the main engine thrust chamber segment support structure design, and effort toward completion of the main and secondary engine turbopump layout drawings. The engine critical component demonstration testing task was primarily directed toward completion of the full main thrust chamber fabrication and assembly. The major fabrication effort was completed, and assembly is in process. The oxidizer pump bearing and seal testing was continued. The main tester was damaged due to the suspected presence of solid contaminant, and the test program was continued with the secondary tester. The final Phase I analysis and design of the propellant feed system was completed by both General Dynamics/Convair and Lockheed Missiles and Space Company. (Author).

MANEUVERING SATELLITE PROPULSION SYSTEM DEMONSTRATION

Author :
Publisher :
ISBN 13 :
Total Pages : 248 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis MANEUVERING SATELLITE PROPULSION SYSTEM DEMONSTRATION by :

Download or read book MANEUVERING SATELLITE PROPULSION SYSTEM DEMONSTRATION written by and published by . This book was released on 1965 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document presents the exploratory development work accomplished in the design, fabrication and testing of advanced rocket engine components for a high-energy-propellant, space maneuvering vehicle. The exploratory development effort consisted of a series of critical experiments to determine operational capabilities of high temperature material and coating in fluorine rich and HF environments, the feasibility of a wide range throttling concept utilizing mixed phase propellants, and the feasibility of an advanced thrust chamber cooling concept.

A rapid method for optimization of the rocket propulsion system for single-stage-to-orbit vehicles

Author : Charles Henry Eldred
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A rapid method for optimization of the rocket propulsion system for single-stage-to-orbit vehicles by : Charles Henry Eldred

Download or read book A rapid method for optimization of the rocket propulsion system for single-stage-to-orbit vehicles written by Charles Henry Eldred and published by . This book was released on 1976 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Reusable Booster System

Author : National Research Council
Publisher : National Academies Press
ISBN 13 : 0309266564
Total Pages : 115 pages
Book Rating : 4.3/5 (92 download)

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Book Synopsis Reusable Booster System by : National Research Council

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.

Modern Engineering for Design of Liquid-Propellant Rocket Engines

Author : Dieter K. Huzel
Publisher : AIAA
ISBN 13 : 9781600864001
Total Pages : 452 pages
Book Rating : 4.8/5 (64 download)

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Book Synopsis Modern Engineering for Design of Liquid-Propellant Rocket Engines by : Dieter K. Huzel

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:

Analysis and Testing of Propellant Feed System Priming Process

Author : T. Y. Lin
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Analysis and Testing of Propellant Feed System Priming Process by : T. Y. Lin

Download or read book Analysis and Testing of Propellant Feed System Priming Process written by T. Y. Lin and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Propulsion Re-Entry Physics

Author : Michał Lunc
Publisher : Elsevier
ISBN 13 : 1483184323
Total Pages : 613 pages
Book Rating : 4.4/5 (831 download)

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Book Synopsis Propulsion Re-Entry Physics by : Michał Lunc

Download or read book Propulsion Re-Entry Physics written by Michał Lunc and published by Elsevier. This book was released on 2014-05-09 with total page 613 pages. Available in PDF, EPUB and Kindle. Book excerpt: Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting maneuvering systems. Problems of re-entry aerodynamics are considered, along with interaction problems in hypersonic fluid dynamics. Comprised of 31 chapters, this volume begins with a detailed account of the quasi-steady adiabatic vaporization and subsequent exothermic decomposition of a pure monopropellant spherical droplet in the absence of free and forced convection. The discussion then turns to results of calculations on MPD machines working in the intermittent and in the continuous mode; inductive plasma accelerators with electromagnetic standing waves; and spherical rocket motors for space and upper stage propulsion. Subsequent chapters focus on pulsed plasma satellite control systems; drag and stability of various Mars entry configurations; hypersonic laminar boundary layers around slender bodies; and effects of an entry probe gas envelope on experiments concerning planetary atmospheres. This book will appeal to students, practitioners, and research workers interested in propulsion re-entry and the accompanying physics.

Advanced Maneuvering Propulsion Technology Program. Volume I. Fluorine/Hydrogen Engine System Analysis and Design

Author : ROCKETDYNE CANOGA PARK CALIF.
Publisher :
ISBN 13 :
Total Pages : 562 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Maneuvering Propulsion Technology Program. Volume I. Fluorine/Hydrogen Engine System Analysis and Design by : ROCKETDYNE CANOGA PARK CALIF.

Download or read book Advanced Maneuvering Propulsion Technology Program. Volume I. Fluorine/Hydrogen Engine System Analysis and Design written by ROCKETDYNE CANOGA PARK CALIF. and published by . This book was released on 1970 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analysis and design studies conducted on the fluorine/hydrogen engine system of the Advanced Maneuvering Propulsion System (AMPS) are presented. The work included the engine system, thrust chamber assemblies, turbopump assemblies, and controls. Design requirements, design tradeoffs, operating characteristics, and layout drawings are shown for the major components and system. (Author).

Advanced Thrust Chamber for Space Maneuvering Propulsion, Task i System Studies

Author : R. P. Pauckert
Publisher :
ISBN 13 :
Total Pages : 283 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Advanced Thrust Chamber for Space Maneuvering Propulsion, Task i System Studies by : R. P. Pauckert

Download or read book Advanced Thrust Chamber for Space Maneuvering Propulsion, Task i System Studies written by R. P. Pauckert and published by . This book was released on 1966 with total page 283 pages. Available in PDF, EPUB and Kindle. Book excerpt: The previous study results of Contract AF04(611)-10745 are extended to investigate the capabilities of increased gross weight Maneuvering Space Propulsion Systems (MSPS) using LF2/LH2, LO2/LH2, and N2O4/N2H4-UDMH(50-50) propellants. The range of stage gross weights considered was based on the payload capabilities of Titan III-C and Saturn I-B and several growth versions of these launch vehicles. Maneuvering space propulsion system gross weights ranging from 20,000 to 50,000 pounds were shown to result in velocity increment capabilities up to 29,000 ft/sec for the 2000-pound payload LF2/LH2 system. The concentric aerodynamic spike/bell engine configuration was selected for the LF2/LH2 and LO2/LH2 system design thrust levels investigated. The configuration selected for the N2O4/N2H4-UDMH(50-50) consisted of one larger primary bell nozzle engine and two small secondary bell nozzle engines. The orbit storage life capabilities of the three propellant combinations were determined and compared for a 20,000-pound-gross weight stage. The LF2/LH2 system provided higher delta V capabilities than the other propellants for orbital storage times up to 2 years with full propellant tanks. The delta V advantage for the LF2/LH2 systems is also maintained when mission duty cycles result in partial propellant loads for the major portion of the storage duration. (Author).

Aerospace Propulsion Systems

Author : Thomas A. Ward
Publisher : John Wiley & Sons
ISBN 13 : 0470824972
Total Pages : 557 pages
Book Rating : 4.4/5 (78 download)

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Book Synopsis Aerospace Propulsion Systems by : Thomas A. Ward

Download or read book Aerospace Propulsion Systems written by Thomas A. Ward and published by John Wiley & Sons. This book was released on 2010-05-17 with total page 557 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerospace Propulsion Systems is a unique book focusing on each type of propulsion system commonly used in aerospace vehicles today: rockets, piston aero engines, gas turbine engines, ramjets, and scramjets. Dr. Thomas A. Ward introduces each system in detail, imparting an understanding of basic engineering principles, describing key functionality mechanisms used in past and modern designs, and provides guidelines for student design projects. With a balance of theory, fundamental performance analysis, and design, the book is specifically targeted to students or professionals who are new to the field and is arranged in an intuitive, systematic format to enhance learning. Covers all engine types, including piston aero engines Design principles presented in historical order for progressive understanding Focuses on major elements to avoid overwhelming or confusing readers Presents example systems from the US, the UK, Germany, Russia, Europe, China, Japan, and India Richly illustrated with detailed photographs Cartoon panels present the subject in an interesting, easy-to-understand way Contains carefully constructed problems (with a solution manual available to the educator) Lecture slides and additional problem sets for instructor use Advanced undergraduate students, graduate students and engineering professionals new to the area of propulsion will find Aerospace Propulsion Systems a highly accessible guide to grasping the key essentials. Field experts will also find that the book is a very useful resource for explaining propulsion issues or technology to engineers, technicians, businessmen, or policy makers. Post-graduates involved in multi-disciplinary research or anybody interested in learning more about spacecraft, aircraft, or engineering would find this book to be a helpful reference. Lecture materials for instructors available at www.wiley.com/go/wardaero

Aerospace Propulsion

Author : T. W. Lee
Publisher : John Wiley & Sons
ISBN 13 : 1118307984
Total Pages : 316 pages
Book Rating : 4.1/5 (183 download)

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Book Synopsis Aerospace Propulsion by : T. W. Lee

Download or read book Aerospace Propulsion written by T. W. Lee and published by John Wiley & Sons. This book was released on 2013-12-31 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerospace propulsion devices embody some of the most advanced technologies, ranging from materials, fluid control, and heat transfer and combustion. In order to maximize the performance, sophisticated testing and computer simulation tools are developed and used. Aerospace Propulsion comprehensively covers the mechanics and thermal-fluid aspects of aerospace propulsion, starting from the fundamental principles, and covering applications to gas-turbine and space propulsion (rocket) systems. It presents modern analytical methods using MATLAB and other advanced software and includes essential elements of both gas-turbine and rocket propulsion systems. Gas turbine coverage includes thermodynamic analysis, turbine components, diffusers, compressors, turbines, nozzles, compressor-turbine matching, combustors and afterburners. Rocket coverage includes chemical rockets, electrical rockets, nuclear and solar sail. Key features: Both gas-turbine and rocket propulsion covered in a single volume Presents modern analytical methods and examples Combines fundamentals and applications, including space applications Accompanied by a website containing MATLAB examples, problem sets and solutions Aerospace Propulsion is a comprehensive textbook for senior undergraduate graduate and aerospace propulsion courses, and is also an excellent reference for researchers and practicing engineers working in this area.