فناوری موشکی بالستیک و هوافضا: مجموعه مقالات ششمین سمپوزیوم فناوری موشکی بالستیک و هوافضا. جلد ۳، پیشرانه، علوم فضایی و اکتشاف فضایی

Ballistic Missile and Aerospace Technology, Volume III: Propulsion, Space Science and Space Exploration covers the proceedings of the Sixth Symposium on Ballistic Missile and Aerospace Technology, held in University of Southern California, Los Angeles, on August 29-31, 1961. This book contains three parts encompassing 18 chapters that explore the components of the propulsion systems, space science and experiments, and exploration of the moon and planets. Part I demonstrates first the advantage of using factorial experimental designs for a wide variety of missile propulsion design problems. This topic is followed by an outline of the component designs of rocket design simulators and a systematic method for determination of ablation rates in a corrosive environment. This part also presents an analysis of the open cycle technique for the removal of afterheat from a nuclear rocket and the design conditions for convergent nozzles. Part II describes the determination of the magnetic dipole of TIROS II, a spin-stabilized meteorological satellite, as well as a method for the acquisition of meteorological data, which provides information not readily available on a global scale and/or in real time. Part III discusses the principles of small payload dropping for space exploration; the geological problems involved in the location of a lunar base; and the features of a planetary entry vehicle. This concluding part also examines the degree of radiation safety resulting from different lunar spacecraft design and mission operations and the feasibility of placing and maintaining space vehicles in the earth-moon libration points. Aerospace engineers and scientists will find this book invaluable. Content: BALLISTIC MISSILE and AEROSPACE TECHNOLOGY , Page ii Front Matter , Page iii Copyright , Page iv CONTRIBUTORS , Pages v-vi PREFACE , Page vii , C.T. Morrow, L.D. Ely, M.R. Smith THE USE OF STATISTICAL DESIGN IN MISSILE PROPULSION STUDIES , Pages 3-18 , C.A. O'Malley COMPARISON OF HIGH-ALTITUDE SIMULATORS FOR ROCKET TESTING , Pages 19-38 , V. Ilsen A PRELIMINARY VEHICLE INSTALLATION STUDY FOR PROJECT SUNFLOWER , Pages 39-71 , J.A. Rudy, D.W. Liechty, J.E. Taylor PRACTICAL DESIGN CONSIDERATIONS AND THEIR IMPLICATIONS FOR HIGH MASS FRACTION, GLASS FILAMENT REINFORCED PLASTIC CASE MOTORS , Pages 73-84 , Jack Elias AUTOGENOUS PRESSURIZATION SYSTEM ANALYSIS OF PROPELLANT TANK PRESSURIZATION , Pages 85-102 , T.F. Morey, M.M. Koshar A SYSTEMATIC METHOD FOR DETERMINATION OF ABLATION RATES IN A CORROSIVE ENVIRONMENT , Pages 103-119 , Eugene P. Bartlett NUCLEAR ROCKET ENGINE AFTERHEAT REMOVAL , Pages 121-135 , R.D. Leonard THE EFFECT OF SECONDARY WASTE HEAT ON SPACE VEHICLE RADIATOR AREA , Pages 137-169 , Calvin C. Silverstein CURVED NOZZLES , Pages 171-203 , V. Ilsen MEASURING THE MAGNETIC DIPOLE OF A SATELLITE , Pages 207-220 , C. Usiskin, R. Wilkes EXTRACTING AND PROCESSING METEOROLOGICAL DATA OBTAINED FROM AN IR/RADAR SATELLITE , Pages 221-246 , Marvin H. Johnson GEOMAGNETIC FIELD PERTURBATIONS DUE TO TRAPPED PARTICLES , Pages 247-264 , J.R. Apel, S.F. Singer DIFFRACTION LIMITATIONS IN DETECTING DISTANT TARGETS BY THEIR SHADOWS , Pages 265-285 , D.I. Caplan EXPLORATION OF THE ATMOSPHERE OF VENUS WITH A SMALL PAYLOAD , Pages 289-309 , Robert L. Sax GEOLOGICAL PROBLEMS IN THE LOCATION OF A LUNAR BASE , Pages 311-339 , John W. Salisbury PLANETARY LANDING AND OBSERVATION PACKAGE , Pages 341-363 , R.W. Clapp, A.T. Owens, R.L. Sax EVALUATION OF SPACE RADIATION SAFETY PROCEDURES IN THE DESIGN AND OPERATION OF SOME EARLY MANNED LUNAR VEHICLES , Pages 365-426 , A.J. Beck, E. Divita, S.L. Russak THE USE OF THE EARTH-MOON LIBRATION POINTS AS TERMINALS FOR SPACE STATIONS , Pages 427-445 , George A. Ellis, Anthony C. Diana