Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Journal of Propulsion Technology》 1989-06
Add to Favorite Get Latest Update

PREDICTING BURNING RATE OF AMMONIUM NITRATE PROPELLANTS

Song Hongchang (Hua Dong Engineering Institute)  
In this paper the decomposition of RDX, HMX and the its influence on burning rate of solid propellants is discussed.A computer program to calculate the burning rate of AP/RDX(HMX)/HTPB(PU)/A1 composition prOpellants is presented. The quantitative predictions by the method under various propellant compositions and solid particle sizes appear to be basically in accordance with the exprimental results.
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved