AN IMPROVED MODEL FOR THE COMBUSTION OF AP COMPOSITE PROPELLANTS

被引：45

作者：

COHEN, NS ^{[1
]}

STRAND, LD ^{[1
]}

机构：

[1] CALTECH,JET PROP LAB,PASADENA,CA 91103

来源：

关键词：

D O I：

10.2514/3.8013

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1739 / 1746

页数：8

共 16 条

[1]

Beckstead M.W., 1977, CPIA PUB 292, P281

[2]

Beckstead M. W., 1981, 18 S INT COMB COMB I, P175

[3]

Beckstead M. W., 1971, 13TH S INT COMB PITT, P1047

[4]

BECKSTEAD MW, 1981, COMMUNICATION

[5]

Beckstead MW., 1970, AIAA J, V8, P2200, DOI [10.2514/3.6087, DOI 10.2514/3.6087]

[6]

BURKE SP, 1965, 1ST 2ND S COMB PITTS, P2

[7] REVIEW OF COMPOSITE PROPELLANT BURN RATE MODELING [J].

COHEN, NS .

[8] ROLE OF BINDERS IN SOLID-PROPELLANT COMBUSTION [J].

COHEN, NS ;

FLEMING, RW ;

DERR, RL .

FENN, JB .

[10]

KING MK, 1978, 16TH AIAA AER SCI M