Shock Radiation Tests for Saturn and Uranus Entry Probes-Reference-Cited by-同舟云学术

Shock Radiation Tests for Saturn and Uranus Entry Probes

Published:2017-11 Issue:6 Volume:54 Page:1246-1257
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Cruden Brett A.¹,Bogdanoff David W.¹

Affiliation:

1. ERC Incorporated at NASA Ames Research Center, Moffett Field, California 94035

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33891

Reference22 articles.

1. National Research Council, Vision and Voyages for Planetary Science in the Decade 2013-2022, National Academies Press, Washington, D.C., 2012, pp. 206–208.

2. Aeroheating Uncertainties in Uranus and Saturn Entries by the Monte Carlo Method

3. Preliminary Convective-Radiative Heating Environments for a Neptune Aerocapture Mission

4. Radiative interaction between driver and driven gases in an arc-driven shock tube

5. CrudenB. A. “Absolute Radiation Measurements in Earth and Mars Entry Conditions,” NATO RTO Lecture Series RTO-EN-AVT-218, 2014.

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