Comparison of theory with atomic oxygen 130.4 nm radiation data from the bow shock ultraviolet 2 rocket flight

Deborah A. Levin; Graham V. Candler; Robert J. Collins; Carl L. Howlett; Patrick Espy; Ellis Whiting; Chul Park

Comparison of theory with atomic oxygen 130.4 nm radiation data from the bow shock ultraviolet 2 rocket flight

Deborah A. Levin, Graham V. Candler, Robert J. Collins, Carl L. Howlett, Patrick Espy, Ellis Whiting, Chul Park

Aerospace Engineering and Mechanics

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

2 Scopus citations

Abstract

Comparison is made between the results obtained from a state-of-the-art flow and radiative model and bow shock vacuum ultraviolet (VUV) data obtained the recent Bow Shock 2 Flight Experiment. An extensive data set was obtained from onboard rocket measurements at a reentry speed of 5 km/sec between the altitudes of approximately 65-85 km. A description of the NO photoionization cell used, the data, and the interpretation of the data will be presented. The primary purpose of the analyses is to assess the utility of the data and to propose a radiation model appropriate to the flight conditions of Bow Shock 2. Theoretical predictions based on flow modeling discussed in earlier work and a new radiation model are compared with data.

Original language	English (US)
Title of host publication	AIAA 28th Thermophysics Conference, 1993
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
State	Published - Jan 1 1993
Event	AIAA 28th Thermophysics Conference, 1993 - Orlando, United States Duration: Jul 6 1993 → Jul 9 1993

Other

Other	AIAA 28th Thermophysics Conference, 1993
Country/Territory	United States
City	Orlando
Period	7/6/93 → 7/9/93

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Comparison of theory with atomic oxygen 130.4 nm radiation data from the bow shock ultraviolet 2 rocket flight. / Levin, Deborah A.; Candler, Graham V.; Collins, Robert J. et al.
AIAA 28th Thermophysics Conference, 1993. American Institute of Aeronautics and Astronautics Inc, AIAA, 1993. AIAA 93-2811.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Levin, DA, Candler, GV, Collins, RJ, Howlett, CL, Espy, P, Whiting, E & Park, C 1993, Comparison of theory with atomic oxygen 130.4 nm radiation data from the bow shock ultraviolet 2 rocket flight. in AIAA 28th Thermophysics Conference, 1993., AIAA 93-2811, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 28th Thermophysics Conference, 1993, Orlando, United States, 7/6/93.

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abstract = "Comparison is made between the results obtained from a state-of-the-art flow and radiative model and bow shock vacuum ultraviolet (VUV) data obtained the recent Bow Shock 2 Flight Experiment. An extensive data set was obtained from onboard rocket measurements at a reentry speed of 5 km/sec between the altitudes of approximately 65-85 km. A description of the NO photoionization cell used, the data, and the interpretation of the data will be presented. The primary purpose of the analyses is to assess the utility of the data and to propose a radiation model appropriate to the flight conditions of Bow Shock 2. Theoretical predictions based on flow modeling discussed in earlier work and a new radiation model are compared with data.",

author = "Levin, {Deborah A.} and Candler, {Graham V.} and Collins, {Robert J.} and Howlett, {Carl L.} and Patrick Espy and Ellis Whiting and Chul Park",

year = "1993",

month = jan,

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language = "English (US)",

booktitle = "AIAA 28th Thermophysics Conference, 1993",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

note = "AIAA 28th Thermophysics Conference, 1993 ; Conference date: 06-07-1993 Through 09-07-1993",

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T1 - Comparison of theory with atomic oxygen 130.4 nm radiation data from the bow shock ultraviolet 2 rocket flight

AU - Levin, Deborah A.

AU - Candler, Graham V.

AU - Collins, Robert J.

AU - Howlett, Carl L.

AU - Espy, Patrick

AU - Whiting, Ellis

AU - Park, Chul

PY - 1993/1/1

Y1 - 1993/1/1

N2 - Comparison is made between the results obtained from a state-of-the-art flow and radiative model and bow shock vacuum ultraviolet (VUV) data obtained the recent Bow Shock 2 Flight Experiment. An extensive data set was obtained from onboard rocket measurements at a reentry speed of 5 km/sec between the altitudes of approximately 65-85 km. A description of the NO photoionization cell used, the data, and the interpretation of the data will be presented. The primary purpose of the analyses is to assess the utility of the data and to propose a radiation model appropriate to the flight conditions of Bow Shock 2. Theoretical predictions based on flow modeling discussed in earlier work and a new radiation model are compared with data.

AB - Comparison is made between the results obtained from a state-of-the-art flow and radiative model and bow shock vacuum ultraviolet (VUV) data obtained the recent Bow Shock 2 Flight Experiment. An extensive data set was obtained from onboard rocket measurements at a reentry speed of 5 km/sec between the altitudes of approximately 65-85 km. A description of the NO photoionization cell used, the data, and the interpretation of the data will be presented. The primary purpose of the analyses is to assess the utility of the data and to propose a radiation model appropriate to the flight conditions of Bow Shock 2. Theoretical predictions based on flow modeling discussed in earlier work and a new radiation model are compared with data.

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M3 - Conference contribution

AN - SCOPUS:85001950544

BT - AIAA 28th Thermophysics Conference, 1993

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - AIAA 28th Thermophysics Conference, 1993

Y2 - 6 July 1993 through 9 July 1993

ER -

Comparison of theory with atomic oxygen 130.4 nm radiation data from the bow shock ultraviolet 2 rocket flight

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