AN IMPROVED MODEL FOR THE COMBUSTION OF AP COMPOSITE PROPELLANTSCOHEN NS; STRAND LD.1982; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 12; PP. 1739-1746; BIBL. 16 REF.Article

EFFECT OF HMX ON THE COMBUSTION RESPONSE FUNCTIONSTRAND LD; COHEN NS.1980; J. SPACE ROCKETS; ISSN 0022-4650; USA; DA. 1980; VOL. 17; NO 6; PP. 566-568; BIBL. 7 REF.Article

THEORETICAL COMBUSTION MODELING STUDY OF NITRAMINE PROPELLANTS.KUMAR RN; STRAND LD.1977; J. SPACEER. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 427-433; BIBL. 18 REF.Article

DETERMINATION OF SOLID-PROPELLANT TRANSIENT REGRESSION RATES USING A MICROWAVE DOPPLER SHIFT TECHNIQUESTRAND LD; SCHULTZ AL; REEDY GK et al.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1118; PP. 1-19; BIBL. 1 P. 1/2Conference Paper