An analytic solution for entry into planetary atmospheres-Reference-Cited by-同舟云学术

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An analytic solution for entry into planetary atmospheres

Published:1965-03 Issue:3 Volume:3 Page:470-475
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

CITRON S. J.¹,MEIR T. C.¹

Affiliation:

1. Purdue University, Lafayette, Ind.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference15 articles.

1. Eggers, A. J., Jr., Alien, H. J., and Neice, S. E. "A comparative analysis of the performance of long-range hypervelocity vehicles/7NACA TN-4046 (1957).

2. Norman, W. S. "Improvements to the Alien and Eggers solution for ballistic re-entry," U. S. Air Force Rept. USAFA-TN63-2(1963).

Cited by 15 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Relative Motion in the Velocity Frame for Atmospheric Entry Trajectories;Journal of Spacecraft and Rockets;2023-09

2. Analytical Assessment of Drag-Modulation Trajectory Control for Planetary Entry;The Journal of the Astronautical Sciences;2018-10-24

3. Review and Assessment of the Steep Lifting Entry Closed-Form Trajectory Solution;AIAA Atmospheric Flight Mechanics Conference;2016-01-01

4. Extension and Enhancement of the Allen–Eggers Analytical Ballistic Entry Trajectory Solution;Journal of Guidance, Control, and Dynamics;2015-03

5. Extension and Enhancement of the Allen-Eggers Analytic Solution for Ballistic Entry Trajectories;AIAA Atmospheric Flight Mechanics Conference;2014-06-13

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