المؤلفون: Schwartz, Daniel F., Merill, Claude E.

المساهمون: AIR FORCE RESEARCH LAB EDWARDS AFB CA SPACE AND MISSILE PROPULSION DIV

المصدر: DTIC AND NTIS

مصطلحات موضوعية: Explosions, Solid Propellant Rocket Engines, Solid Rocket Propellants, Guided Missiles, HAZARDS, ROCKET ENGINES, SYMPATHETIC DETONATIONS, SOLID ROCKET PROPELLANTS, INTERCONTINENTAL BALLISTIC MISSILES, TEST AND EVALUATION, SCENARIOS, COMPOSITE STRUCTURES, IMPACT SHOCK, ROCKET ENGINE CASES, THIRD STAGE ENGINES, PROPELLANT TANKS, TANK FRAGMENTS, HYDROXY TERMINATED POLYBUTADIENE, SICBM(SMALL INTERCONTINENTAL BALLISTIC MISSILES), SDT(SHOCK TO DETONATION TRANSITION), FIRST STAGE ENGINES, WUAFRL48470122

وصف الملف: text/html

Relation: http://www.dtic.mil/docs/citations/ADA423229

الاتاحة: http://www.dtic.mil/docs/citations/ADA423229
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA423229

المؤلفون: AIR FORCE RESEARCH LAB EDWARDS AFB CA SPACE AND MISSILE PROPULSION DIV, Schwartz, Daniel F., Merill, Claude E.

المصدر: DTIC AND NTIS

مصطلحات الفهرس: Explosions, Solid Propellant Rocket Engines, Solid Rocket Propellants, Guided Missiles, HAZARDS, ROCKET ENGINES, SYMPATHETIC DETONATIONS, SOLID ROCKET PROPELLANTS, INTERCONTINENTAL BALLISTIC MISSILES, TEST AND EVALUATION, SCENARIOS, COMPOSITE STRUCTURES, IMPACT SHOCK, ROCKET ENGINE CASES, THIRD STAGE ENGINES, PROPELLANT TANKS, TANK FRAGMENTS, HYDROXY TERMINATED POLYBUTADIENE., SICBM(SMALL INTERCONTINENTAL BALLISTIC MISSILES), SDT(SHOCK TO DETONATION TRANSITION), FIRST STAGE ENGINES, WUAFRL48470122, Text

URL: https://apps.dtic.mil/docs/citations/ADA423229