Influence of Ablation on Radiative Heating for Earth Entry-Reference-Cited by-同舟云学术

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Influence of Ablation on Radiative Heating for Earth Entry

Published:2009-05 Issue:3 Volume:46 Page:481-491
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Johnston Christopher O.¹,Gnoffo Peter A.¹,Sutton Kenneth²

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

2. National Institute of Aerospace, Hampton, Virginia 24060

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.40290

Reference96 articles.

1. C Lines 0-18 [48,59,60] Photoionization 0-18 [50]

2. H Lines 0-18 [48,61] Photoionization 0-18 [50]

3. CO 4 A1X1 6.0-10 [62] 3 b3a3 3.0-5.0 [62] B1X110.2-11.4 [63] C1X110.0-12.2 [63] E1X111.2-11.9 [63]

4. Angstrom (B1A1) 0.5-3.2 [62] Asundi (a3a3) 0.1-3.5 [62] Triplet (d3a3) 0.1-4.0 [62]

5. C2 Swan (d3a3) 0.4-4.2 [62] Phillips (A1X1) 0.1-2.7 [62]

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