Research And Investigation Of A Resistance Jet Attitude Control System
DOWNLOAD
Download Research And Investigation Of A Resistance Jet Attitude Control System PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Research And Investigation Of A Resistance Jet Attitude Control System book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Research And Investigation Of A Resistance Jet Attitude Control System
DOWNLOAD
Author : R. C. Wells
language : en
Publisher:
Release Date : 1966
Research And Investigation Of A Resistance Jet Attitude Control System written by R. C. Wells and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.
This report summarizes a research and development program for the use of a Resistance Jet Attitude Control in space vehicles and earth-orbiting satellites. The work was primarily concerned with the development and evaluation of basic components and establishing system and component design criteria. The overall effort included work in three general areas: (1) An analysis of missions and vehicles suitable for use of the resistance jet and a selection for subsequent work. (2) The analysis of various control logic techniques, a comparison and selection of the method most suitable for use with the resistance jet, and the building and evaluation of breadboard electronics. (3) Development of the resistance jet thruster was accomplished in two stages, a preliminary thruster and a prototype thruster. The preliminary engine was built and evaluated, the design was revised and two prototype engines were built and tested. Correlation between theory and test was demonstrated. A measure of system performance was obtained by an analog tie-in of the breadboard electronics and simulated thruster operation. (Author).
A Resistance Jet Attitude Control System And A Control Logic For Attitude Control Of A Space Vehicle
DOWNLOAD
Author : Cornett Eugene Hall (CAPT, USAF.)
language : en
Publisher:
Release Date : 1966
A Resistance Jet Attitude Control System And A Control Logic For Attitude Control Of A Space Vehicle written by Cornett Eugene Hall (CAPT, USAF.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.
Technical Abstract Bulletin
DOWNLOAD
Author :
language : en
Publisher:
Release Date :
Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.
A Reaction Attitude Control System For Jet Vtol Research Aircraft
DOWNLOAD
Author : Frank A. Pauli
language : en
Publisher:
Release Date : 1970
A Reaction Attitude Control System For Jet Vtol Research Aircraft written by Frank A. Pauli and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aircraft categories.
Rapid air switching and low torque nozzle for dual reaction attitude control for jet VTOL aircraft.
Nasa Technical Memorandum
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1986
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with Aeronautics categories.
Collection Of Technical Papers
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1969
Collection Of Technical Papers written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aeronautics categories.
A Reaction Attitude Control System For Jet Vtol Research Aircraft
DOWNLOAD
Author : Frank A. Pauli
language : en
Publisher:
Release Date : 1970
A Reaction Attitude Control System For Jet Vtol Research Aircraft written by Frank A. Pauli and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Airplanes categories.
"A new dual reaction control system provides the means for flight research on the requirements for VTOL attitude control systems. There are two conflicting requirements for any control system used in flight research. One is flexibility and the other is safety. Maximum flexibility can best be achieved by an electrically driven control system, but this frequently degrades safety. Maximum safety is provided by a mechanical control system. But this type system is difficult to change or adjust. Pilots consider their safety is not endangered if it is possible to switch from an electrical drive system to a mechanical drive system in about 0.1 sec after an electrical failure. The new dual reaction control system satisfies this requirement with a fail safe air switching system that controls 8.5 lb-m/sec of 500° F air. The research control system is an electrical drive system. The air switching concept set the requirement for large reaction control nozzles to handle the required air flow without excessive losses. Large nozzles, however, require large driving torques, although some nozzle types have lower driving torque requirements than others. An experimental determination was made for several reaction nozzle concepts to find the type with the lowest torque requirement. An outside can-type was devised that had sufficiently low driving torques (290 in.-oz for 60 psig air using a 3 sq in. exit area) so that a low power and low weight servomotor could be used and still achieve high response. It was also found that additional lift could be developed by a variation in this type nozzle. The combination of concepts of a rapid switching valve and a low torque nozzle permit maximum flexibility in system design of reaction attitude control systems for jet VTOL research aircraft."--P. [i].
Investigation Of A Pitch Attitude Control System For Some Representative Transonic And Supersonic Aircraft
DOWNLOAD
Author : William V. Caldwell
language : en
Publisher:
Release Date : 1954
Investigation Of A Pitch Attitude Control System For Some Representative Transonic And Supersonic Aircraft written by William V. Caldwell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerodynamics, Supersonic categories.
Scientific And Technical Aerospace Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date :
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Aeronautics categories.
Star
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1973
Star written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with Aeronautics categories.