Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 5 Vehicle Design
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Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 5 Vehicle Design
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Author :
language : en
Publisher:
Release Date : 1968
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 5 Vehicle Design written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
A parametric analysis of a broad spectrum of thermostructural concepts is presented. A complete structural concept for the 35-foot entry test vehicle using the FDL-5 configuration is defined. Subsystems for the entry test vehicle are selected. A weight breakdown and a weight summary for the test vehicle are presented.
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 2 Parametric Configuration Development And Evaluation
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Author :
language : en
Publisher:
Release Date : 1968
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 2 Parametric Configuration Development And Evaluation written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
The derivation of two volumetric efficient high L/D entry vehicles is described. Parametric trades in the areas of aerodynamics and aerothermodynamics are discussed and selected parameters are identified. Alternate modes of vehicle recovery are described and the effect on vehicle design determined. The evolution of the FDL-5 configuration selected for wind tunnel testing is described through the presentation of a series of intermediate configurations.
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 4 Aerothermodynamics
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Author :
language : en
Publisher:
Release Date : 1968
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 4 Aerothermodynamics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
Design and experimental analyses of unmanned entry research vehicles having high hypersonic L/D and high volume are described. Analytic parametric data are presented for two lifting body classes designated HLD-35 and FDL-5. Experimental aerodynamic and heat transfer data obtained from Arnold Engineering Development Wind Tunnels A, B, C, and F are compared with analytic data for the FDL-5 vehicle. Structure and subsystems are selected for performing unmanned hypersonic research with the vehicle.
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part I Summary
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Author :
language : en
Publisher:
Release Date : 1968
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part I Summary written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
Conceptual design and experimental wind tunnel testing of unmanned entry research vehicles having high hypersonic lift/drag ratio and high volume are described. Analytic parametric data are presented for two lifting body classes designated HLD-35 and FDL-5. The FDL-5 is a unique configuration which is aerodynamically stabilized without outboard fins. Experimental aerodynamic and heat transfer fata from the Arnold Engineering Development Center Wind Tunnels A, B, C, and F are compared with analytic data for the FDL-5. Candidate structure and subsystems are selected for performing unmanned hypersonic research with the vehicle. (Author).
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft
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Author : F. L. Guard
language : en
Publisher:
Release Date : 1968
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft written by F. L. Guard and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Aerodynamics, Hypersonic categories.
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 3 Aerodynamics
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Author :
language : en
Publisher:
Release Date : 1968
Preliminary Design And Experimental Investigation Of The Fdl 5a Unmanned High L D Spacecraft Part 3 Aerodynamics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
The aerodynamic wind tunnel test program for the FDL-5 configuration is described in this Part III. The description includes the models, test facilities, data reduction and presentation, and the test schedules. A complete presentation of the aerodynamic test data is provided. The data include six component force and moment data, pressure data, and photographic data for the Mach number range between 1.5 to 20. Correlations between the data and appropriate theories are presented. The overall aerodynamic characteristics of the FDL-5 configuration are defined.
Preliminary Design Of A Modular Unmanned Research Vehicle
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Author : Christopher Dean Hall
language : en
Publisher:
Release Date : 1988
Preliminary Design Of A Modular Unmanned Research Vehicle written by Christopher Dean Hall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with Vehicles, Remotely piloted categories.
Preliminary Design Of A Modular Unmanned Research Vehicle Volume 1 System Design Document
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Author : Christopher D. Hall
language : en
Publisher:
Release Date : 1988
Preliminary Design Of A Modular Unmanned Research Vehicle Volume 1 System Design Document written by Christopher D. Hall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with categories.
This thesis presents the analysis and development of a modular unmanned research vehicle (MURV) to support aeronautical research for AFIT. The MURV is proposed as a test vehicle to permit experimental efforts beyond the restrictions of pure analytical and wind tunnel research, yet less costly and more accessible than full-scale flight tests. A classical systems approach was applied in concert with a conventional aircraft design process which emphasized system level needs and objectives in the design of MURV subsystems. The primary design drivers were the need for adequate data acquisition for anticipated experiments, structural and functional modularity to permit simple reconfiguration, and focus on a set of unique experiments relating to fighter-like supermaneuverability. The supermaneuverability experiments dictated that the general arrangement of the MURV baseline design would resemble a typical modern fighter aircraft configuration, the recommended baseline being a turbojet-powered delta wing design with canards, single vertical tail, and control-configured ventral fins. Modularity implications resulted in the design of a flexible, digital flight control system with primary functions distributed between the vehicle and a remote pilot/control ground station, and a fuselage design which allows for relocation and replacement of wings and tails or canards. The data acquisition system is fully integrated with the flight control system and the remote ground station. The MURV is capable of flight speeds approaching 260 knots for altitudes up to 20,000 feet, and has fuel to fly for well over 30 minutes. (edc).
Preliminary Design Of A Modular Unmanned Research Vehicle Volume 2 Subsystem Technical Development Design Study
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Author : Christopher D. Hall
language : en
Publisher:
Release Date : 1988
Preliminary Design Of A Modular Unmanned Research Vehicle Volume 2 Subsystem Technical Development Design Study written by Christopher D. Hall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with categories.
This thesis presents the analysis and development of a modular unmanned research vehicle (MURV) to support AFIT's aeronautical research. The MURV is proposed as a test vehicle to permit experimental efforts beyond the restrictions of pure analytical and wind tunnel research, yet less costly and more accessible than full-scale flight tests. A classical systems approach was applied, in concert with a conventional aircraft design process, which emphasized system level needs and objectives in the design of MURV subsystems. Primary design drivers were the need for adequate data acquisition for anticipated experiments, structural and functional modularity to permit simple reconfiguration, and focus on a set of unique experiments relating to fighter-like supermaneuverability. The supermaneuverability experiments dictated that the general arrangement of the MURV baseline design would resemble a typical modern fighter aircraft configuration, the recommended baseline being a turbojet-powered delta wing design with canards, single vertical tail, and control-configured ventral fins. Modularity implications resulted in the design of a flexible, digital flight control system with primary functions distributed between the vehicle and a remote pilot/control ground station and a fuselage design which allows for relocation and replacement of wings and tails or canards. The data acquisition system is fully integrated with the flight control system and the remote ground station. The MURV is capable of flight speeds approaching 260 knots for altitudes up to 20,000 feet, and has fuel to fly for over 30 mins. Theses. (EDC).
Manned Spacecraft Design Principles
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Author : Pasquale M Sforza
language : en
Publisher: Butterworth-Heinemann
Release Date : 2015-11-19
Manned Spacecraft Design Principles written by Pasquale M Sforza and has been published by Butterworth-Heinemann this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-11-19 with Business & Economics categories.
Manned Spacecraft Design Principles presents readers with a brief, to-the-point primer that includes a detailed introduction to the information required at the preliminary design stage of a manned space transportation system. In the process of developing the preliminary design, the book covers content not often discussed in a standard aerospace curriculum, including atmospheric entry dynamics, space launch dynamics, hypersonic flow fields, hypersonic heat transfer, and skin friction, along with the economic aspects of space flight. Key concepts relating to human factors and crew support systems are also included, providing users with a comprehensive guide on how to make informed choices from an array of competing options. The text can be used in conjunction with Pasquale Sforza's, Commercial Aircraft Design Principles to form a complete course in Aircraft/Spacecraft Design.