Titlebook: Re-entry and Planetary Entry Physics and Technology; I / Dynamics, Physic W. H. T. Loh,W. H. T. Loh Book 1968 Springer-Verlag New York Inc.

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978-3-642-48929-7Springer-Verlag New York Inc. 1968

細(xì)頸瓶

Re-entry and Planetary Entry Physics and Technology978-3-642-48927-3Series ISSN 0066-5509

CRASS

ARY

Entry Radiative Transferdominant part of the heat load to be withstood by the ablative surface. Kivel. compared convective and radiative heat loads for an ICBM entering at about 20,000 ft/sec and for a Mars probe entering at about 40,000 ft/sec. Figures 5-1 and 5-2 are sketched from Kivel’s paper:

compassion

Entry Mechanics and DynamicsThe equations of motion of a vehicle entering a planet’s atmosphere have been derived by many authors. We shall use them in the form given by Lees, et al. (Ref. 8).

Prognosis

ETHER

Carl Gazley Jr.ced to the country through the trading operations of the British East India Company and spread through religious and educational activities from the early nineteenth century on. Until the country achieved her independence from British rule in 1957, the greatest social and economic advantages came wi

botany

Summary Discussion on Re-entry and Planetary Entry—Physics and Technologyeration, aerodynamic heating and control of the time and location of landing. For non-atmospheric planets, the problem essentially involves only deceleration and control of the time and location of landing. A general description of atmospheric and non-atmospheric planetary entry precedes the analyses of the problem.