Classification and assessment of solid propellant rocket exhaust signature

Hong Jun Mo; Ning Fei Wang

Classification and assessment of solid propellant rocket exhaust signature

Hong Jun Mo^*, Ning Fei Wang

^*Corresponding author for this work

Xi'an Modern Chemistry Research Institute

Research output: Contribution to journal › Article › peer-review

7 Citations (Scopus)

Abstract

Foreign classification standard of low-signature solid propellants and classification and measurement technique of solid rocket exhaust signatures are presented. The definition, cause of formation, influence on application, theoretical assessment, test methods and equipments for the motor exhaust signature are described and the development direction of measurement and assessment of plume signature are predicted.

Original language	English
Pages (from-to)	229-232
Number of pages	4
Journal	Guti Huojian Jishu/Journal of Solid Rocket Technology
Volume	27
Issue number	3
Publication status	Published - Sept 2004
Externally published	Yes

Keywords

Plume
Signature
Solid propellant
Solid propellant rocket engine

Cite this

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title = "Classification and assessment of solid propellant rocket exhaust signature",

abstract = "Foreign classification standard of low-signature solid propellants and classification and measurement technique of solid rocket exhaust signatures are presented. The definition, cause of formation, influence on application, theoretical assessment, test methods and equipments for the motor exhaust signature are described and the development direction of measurement and assessment of plume signature are predicted.",

keywords = "Plume, Signature, Solid propellant, Solid propellant rocket engine",

author = "Mo, {Hong Jun} and Wang, {Ning Fei}",

year = "2004",

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journal = "Guti Huojian Jishu/Journal of Solid Rocket Technology",

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TY - JOUR

T1 - Classification and assessment of solid propellant rocket exhaust signature

AU - Mo, Hong Jun

AU - Wang, Ning Fei

PY - 2004/9

Y1 - 2004/9

N2 - Foreign classification standard of low-signature solid propellants and classification and measurement technique of solid rocket exhaust signatures are presented. The definition, cause of formation, influence on application, theoretical assessment, test methods and equipments for the motor exhaust signature are described and the development direction of measurement and assessment of plume signature are predicted.

AB - Foreign classification standard of low-signature solid propellants and classification and measurement technique of solid rocket exhaust signatures are presented. The definition, cause of formation, influence on application, theoretical assessment, test methods and equipments for the motor exhaust signature are described and the development direction of measurement and assessment of plume signature are predicted.

KW - Plume

KW - Signature

KW - Solid propellant

KW - Solid propellant rocket engine

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M3 - Article

AN - SCOPUS:10944250648

SN - 1006-2793

VL - 27

SP - 229

EP - 232

JO - Guti Huojian Jishu/Journal of Solid Rocket Technology

JF - Guti Huojian Jishu/Journal of Solid Rocket Technology

IS - 3

ER -

Classification and assessment of solid propellant rocket exhaust signature

Abstract

Keywords

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