Accession Number:

AD0631293

Title:

SPACECRAFT UTILIZING THE LIFTING REENTRY TECHNIQUE. PART II. REVIEW OF THEORETICAL STUDIES IN LIFTING REENTRY

Descriptive Note:

Rept. no. 1 on ATD work assignment no. 52

Corporate Author:

LIBRARY OF CONGRESS WASHINGTON DC AEROSPACE TECHNOLOGY DIV

Report Date:

1966-04-01

Pagination or Media Count:

382.0

Abstract:

This report comprehensive report with annotated bibliography is based on Soviet-Satellite open sources published 1957-1964, although some earlier articles are included. Section I is a comprehensive review of sources on theoretical and experimental studies of problems in fields of space sciences, i.e., problems of lifting and ballistic hypervelocity flight, and atmospheric reentry techniques. There are four parts following the Introduction Group A. High-speed aerodynamics and gas dynamics Group B. High-speed aerothermodynamics Group C. High-speed flight mechanics Group D. Strength of flight -vehicle components thin and sandwich plates and shells. A brief conclusion is given. In writing this report articles and monographs having a closer relation to the reentry problem and showing either an original approach to the problem or a new method applied to its solution were selected from the bibliography and used. Section II is an annotated bibliography containing 861 entries arranged by subject in a manner similar to Section I Group A. aeromechanics of high-speed flows 451 entries Group B. Aerothermodynamics of high-speed flows 168 entries Group C. Flight mechanics 53 entries Group D. Strength of space vehicle components 175 entries Group E. Miscellaneous 14 entries. Translator

Subject Categories:

  • Aerodynamics
  • Astronautics
  • Spacecraft Trajectories and Reentry

Distribution Statement:

APPROVED FOR PUBLIC RELEASE