Combustion effects of C60 soot in ammonium nitrate propellants

被引：16

作者：

Greiner, BE ^{[1
]}

Frederick, RA

Moser, MD

机构：

[1] Sparta Syst Inc, Huntsville, AL 35801 USA

[2] Univ Alabama, Dept Mech & Aerosp Engn, Huntsville, AL 35899 USA

来源：

JOURNAL OF PROPULSION AND POWER | 2003年 / 19卷 / 04期

关键词：

521.1 Fuel Combustion - 523 Liquid Fuels - 537.1 Heat Treatment Processes - 804 Chemical Products Generally - 804.2 Inorganic Compounds;

D O I：

10.2514/2.6161

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Combustion effects of C60 soot in ammonium nitrate propellants was studied. The use of fullerene in an An-based propellant that could provide an increase in burning rate in the same manner as the carbon addition was proposed. The results showed that the fullerene soot has an initiation temperature of 390°C, which was lower than both carbon black and pure fullerene.

引用

页码：713 / 715

页数：3

共 8 条

[1]

BILLHEIMER JS, 1951, 1098992 AER ENG CORP

[2]

Cauty F, 1994, NONINTRUSIVE COMBUST

[3]

CLARKE RP, 1952, METHODS INCREASING B, V33, P21837

[4] Direct ultrasonic measurement of solid propellant ballistics [J].

Di Salvo, R ;

Dauch, F ;

Frederick, RA ;

Moser, MD .

REVIEW OF SCIENTIFIC INSTRUMENTS, 1999, 70 (11) :4416-4421

[5]

GLAZKOVA AP, 1983, FIZ GORENIJA VZRYVA, V19, P65

[6]

GREINER BE, 1996, 963275 AIAA

[7] THERMAL IGNITION STUDIES ON METALLIZED FUEL-OXIDIZER SYSTEMS [J].

JAIN, SR ;

OOMMEN, C .

JOURNAL OF THERMAL ANALYSIS, 1989, 35 (04) :1119-1128

[8]

TALLEY SK, 1954, JANNAF 10 M B, V1, P279

← 1 →