Titlebook: Re-entry and Planetary Entry Physics and Technology; II / Advanced Concep W. H. T. Loh,W. H. T. Loh Book 1968 Springer Science+Business Med

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Book 1968he student, engineer and scientist. The purpose of offering this course is to make available to them these recent significant advances in physics and technology. Accordingly, this course is organized into five parts: Part 1, Entry Dynamics, Thermodynamics, Physics and Radiation; Part 2, Entry Abla-

surmount

Lifting Entry Concepts simple and clear requirements, the first manned orbital vehicles were developed by straightforward extensions of ICBM technology. This growth pattern now appears to be changing as the requirements for future systems become less clearly defined and, at the same time, become much more diverse and complex.

土產(chǎn)

Entry Propulsion and Lower Systems Technologythis time span. Finally, the matrix of these vehicles and mission needs defines— in a broad way—the general requirements and constraints which should be met by future power and propulsion systems for such vehicles.

ciliary-body

Guidance and Control for Atmospheric Entrye important elements in any recentry system, whether it be manned or unmanned. This chapter examines the concepts and hardware for guidance and control of the Mercury, Gemini, and Apollo spacecraft. The reentry technology for manned spacecraft systems has matured very greatly in the 1960’s.

有斑點

Dynamics of Planetary Approachcerned mainly with the third phase dealing with the dynamics of planetary approach. In particular we will consider the Earth-Mars journey, in which case the approach trajectory is computed on the two-body Spacecraft-Mars assumption.

Arresting

Aggregate

Entry Flight Research and Experimentationthis effort is through the use of rocket-propelled, free-flight models. Heat-transfer investigations are needed at high velocities with the high enthalpy conditions of flight in the real environment which rocket models provide. Rocket model investigations are therefore needed to confirm or evaluate

Noctambulant

Lifting Entry Conceptsn years. This has been accomplished through a combination of clearly defined requirements and a national research and development effort. With similar simple and clear requirements, the first manned orbital vehicles were developed by straightforward extensions of ICBM technology. This growth pattern

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