Radiation effects on 1-D ignition transient analysis of SRM

S. T. Chang; S. Han; John C. Chai

doi:10.2514/6.1996-3055

Radiation effects on 1-D ignition transient analysis of SRM

S. T. Chang, S. Han, John C. Chai

Research output: Contribution to conference › Paper › peer-review

9 Citations (Scopus)

Abstract

This paper examines the effects of radiation on the ignition transients of a small SRM with a rear ignition system. Radiation effects become important when the combustion gas absorbs and scatters radiation beams. Their effects appear in terms of radiative heat transfer to the solid propellent during the flame spreading period and radiative energy transfer through ihe combustion gas along the combustion chamber. It is found that the radiation significantly shortens the flame spreading time and alters the behavior of total thrust during the ignition period.

Original language	English
Pages	1-9
Number of pages	9
DOIs	https://doi.org/10.2514/6.1996-3055
Publication status	Published - 1996
Externally published	Yes
Event	32nd Joint Propulsion Conference and Exhibit, 1996 - Lake Buena Vista, United States Duration: Jul 1 1996 → Jul 3 1996

Conference

Conference	32nd Joint Propulsion Conference and Exhibit, 1996
Country/Territory	United States
City	Lake Buena Vista
Period	7/1/96 → 7/3/96

ASJC Scopus subject areas

Energy Engineering and Power Technology
Electrical and Electronic Engineering
Mechanical Engineering
Control and Systems Engineering
Aerospace Engineering

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10.2514/6.1996-3055

Cite this

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title = "Radiation effects on 1-D ignition transient analysis of SRM",

abstract = "This paper examines the effects of radiation on the ignition transients of a small SRM with a rear ignition system. Radiation effects become important when the combustion gas absorbs and scatters radiation beams. Their effects appear in terms of radiative heat transfer to the solid propellent during the flame spreading period and radiative energy transfer through ihe combustion gas along the combustion chamber. It is found that the radiation significantly shortens the flame spreading time and alters the behavior of total thrust during the ignition period.",

author = "Chang, {S. T.} and S. Han and Chai, {John C.}",

note = "Publisher Copyright: {\textcopyright} 1996 American Institute of Aeronautics and Astronautics, Inc.; 32nd Joint Propulsion Conference and Exhibit, 1996 ; Conference date: 01-07-1996 Through 03-07-1996",

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AU - Han, S.

AU - Chai, John C.

PY - 1996

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N2 - This paper examines the effects of radiation on the ignition transients of a small SRM with a rear ignition system. Radiation effects become important when the combustion gas absorbs and scatters radiation beams. Their effects appear in terms of radiative heat transfer to the solid propellent during the flame spreading period and radiative energy transfer through ihe combustion gas along the combustion chamber. It is found that the radiation significantly shortens the flame spreading time and alters the behavior of total thrust during the ignition period.

AB - This paper examines the effects of radiation on the ignition transients of a small SRM with a rear ignition system. Radiation effects become important when the combustion gas absorbs and scatters radiation beams. Their effects appear in terms of radiative heat transfer to the solid propellent during the flame spreading period and radiative energy transfer through ihe combustion gas along the combustion chamber. It is found that the radiation significantly shortens the flame spreading time and alters the behavior of total thrust during the ignition period.

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T2 - 32nd Joint Propulsion Conference and Exhibit, 1996

Y2 - 1 July 1996 through 3 July 1996

ER -

Radiation effects on 1-D ignition transient analysis of SRM

Abstract

Conference

ASJC Scopus subject areas

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