REINFORCEMENT OF COMPOSITE ROCKET PROPELLANTS BY COTTON AND NITROCELLULOSE FIBRES
MOSTAFA, H., HASSANIEN, S., RADWAN, M., SADEK, M. (1997). REINFORCEMENT OF COMPOSITE ROCKET PROPELLANTS BY COTTON AND NITROCELLULOSE FIBRES. EKB Journal Management System, 7(ASAT Conf. 13-15 May 1997), 1-11. doi: 10.21608/asat.1997.25456
H. E. MOSTAFA; S. M. HASSANIEN; M. A. RADWAN; M. A. SADEK. "REINFORCEMENT OF COMPOSITE ROCKET PROPELLANTS BY COTTON AND NITROCELLULOSE FIBRES". EKB Journal Management System, 7, ASAT Conf. 13-15 May 1997, 1997, 1-11. doi: 10.21608/asat.1997.25456
MOSTAFA, H., HASSANIEN, S., RADWAN, M., SADEK, M. (1997). 'REINFORCEMENT OF COMPOSITE ROCKET PROPELLANTS BY COTTON AND NITROCELLULOSE FIBRES', EKB Journal Management System, 7(ASAT Conf. 13-15 May 1997), pp. 1-11. doi: 10.21608/asat.1997.25456
MOSTAFA, H., HASSANIEN, S., RADWAN, M., SADEK, M. REINFORCEMENT OF COMPOSITE ROCKET PROPELLANTS BY COTTON AND NITROCELLULOSE FIBRES. EKB Journal Management System, 1997; 7(ASAT Conf. 13-15 May 1997): 1-11. doi: 10.21608/asat.1997.25456

REINFORCEMENT OF COMPOSITE ROCKET PROPELLANTS BY COTTON AND NITROCELLULOSE FIBRES

International Conference on Aerospace Sciences and Aviation Technology
Article 59, Volume 7, ASAT Conf. 13-15 May 1997, May 1997, Page 1-11  XML PDF (2.33 MB)
Document Type: Original Article
DOI: 10.21608/asat.1997.25456
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Authors
H. E. MOSTAFA1; S. M. HASSANIEN2; M. A. RADWAN3; M. A. SADEK4
1Assistant Lecturer. Explosive Dpt. MTC. Cairo. Egypt.
2Assistant Professor. Head Of The Chem. Eng. Branch. MTC. Cairo. Egypt.
3Assistant Professor. Head Of The Explosive Dpt., MTC. Cairo. Egypt.
4Professor. Ex Head Of Chem. Eng. Branch. MTC. Cat! J. Egypt.
Abstract
The Egyptian extra long stapled cotton "GIZA76" which has a very good mechanical and chemical properties [I] was selected as a raw material to obtain nitrocellulose energetic fibres, such fibres can be used as a reinforcing agent in propellant formulations instead of inert fibres to improve not oniy the mechanical properties of composite propellants but also, the burning rate of such propellant . The effect of either chopped or nonchopped nitrocellulose fibres length and content on the mechanical properties of the prepared propellant samples were examined .Also, the effect of bonding agent on the reinforcing fibres has been investigated .Satisfactory results have been obtained.
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