Download PDF by Claus Weiland: Aerodynamic Data of Space Vehicles

By Claus Weiland

ISBN-10: 3642541674

ISBN-13: 9783642541674

ISBN-10: 3642541682

ISBN-13: 9783642541681

The means and caliber of the atmospheric flight functionality of area flight autos is characterised via their aerodynamic info bases. a whole aerodynamic facts base could surround the coefficients of the static longitudinal and lateral motions and the similar dynamic coefficients.

In this ebook the aerodynamics of 27 autos are thought of. just a couple of of them did rather fly. accordingly the aerodynamic info bases are usually now not entire, particularly while the tasks or courses have been roughly without warning stopped, frequently as a result of political judgements. Configurational layout reviews or the improvement of demonstrators
usually take place with lowered or incomplete aerodynamic facts units. consequently a few facts units base simply at the program of 1 of the subsequent instruments: semi-empirical layout equipment, wind tunnel assessments, numerical simulations. In to this point a excessive percent of the information offered is incomplete and must be verified.

Flight mechanics wishes the aerodynamic coefficients as functionality of loads of variables. The allocation of the aerodynamic coefficients for a selected flight operation at a particular trajectory element is carried out via an aerodynamic version. The institution of such types is defined during this book.

This publication is written for graduate and doctoral scholars to offer them perception into the aerodynamics of some of the flight configurations. extra for layout and improvement engineers in and at learn institutes (including universities) looking for a suitable motor vehicle form, in addition to for non-specialists, who could be in
this topic. The publication may be necessary, too, within the case that method experiences require of their suggestion levels the choice of compatible automobile shapes.

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Additional resources for Aerodynamic Data of Space Vehicles

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After the first triumphant Moon landing further lunar missions (APOLLO 12,14,15,16,17) were conducted. The lunar program was ended with the successful flight of APOLLO 17 in December 1972. There is no doubt that the aerodynamics of the APOLLO capsule are one of the best known. Due to the large number of flights in the 1960s and 1970s either in low Earth orbit or to the Moon, the free flight data base is remarkable. During the design of APOLLO, most of the aerodynamic data was obtained from wind tunnel tests, [3] - [7].

All of the capsules, which have transported and still transport men to and from space, were and are single-use vehicles, launched vertically on top of rockets. The landing, either at sea or on ground, is usually performed with the aid of a parachute system. Although the above-mentioned systems represent reliable means of space transportation, the cost of delivering payloads into space remains much too high and a launch on demand is not possible. Consequently, at the end of the 1980s and during the 1990s, numerous activities all over the world aimed for the developments of fully reusable space transportation systems.

Details of aerodynamics: page 253 ff. 9. Fig. 24. Technology demonstrator vehicle • Germany’s configurational study, • some experimental and numerical data available, • demonstration flights: SHEFEX I in 2005 and SHEFEX II, in 2012, no flight of DS6, • project: begin in the 1990s, • some aerodynamic data of steady motion (longitudinal) available, • dynamic stability data not available. Details of aerodynamics: page 264 ff. 10. Fig. 25. Technology demonstrator vehicle • Italy’s flight demonstrator program, • experimental and numerical data for transonic flight available, • one transonic demonstrator flight in Feb.

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Aerodynamic Data of Space Vehicles by Claus Weiland


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