Development of ammonium perchlorate + aluminium base solid propellant [electronic resource] /

Development of ammonium perchlorate + aluminium base solid propellant [electronic resource] /

Project Paper (Sarjana Muda Kejuruteraan (Mekanikal - Aeronautik)) - Universiti Teknologi Malaysia, 2009

Bibliographic Details
Main Authors:	Norazila Othman, 1985-, Fakulti Kejuruteraan Mekanikal
Format:
Language:	eng
Published:	2009
Subjects:	Solid propellant rockets

Similar Items

Development of ammonium perchlorate + aluminium base solid propellant /
by: Norazila Othman, 1985-, et al.
Published: (2009)

Combustion characteristics of ammonium perchlorate based solid rocket propellant [electronic resource] /
by: 326806 Amir Aziz, et al.
Published: (2011)

Combustion characteristics of ammonium perchlorate based solid rocket propellant /
by: 326806 Amir Aziz, et al.
Published: (2011)

To develop solid propellant based on kno3 with carbon mixture [electronic resource] /
by: 184169 Mohd. Qayyam Omar, et al.
Published: (2008)

Study on the influence of grain shape on solid propellant performance [electronic resource] /
by: Mohd. Muzamil Wahab, 1984-
Published: (2008)

Study on the influence of grain shape on solid propellant performance /
by: Mohd. Muzamil Wahab, 1984-, et al.
Published: (2008)

Development of pressurised burning rate test rig for solid propellant [electronic resource] /
by: 428135 Nasrulhakim Musa, et al.
Published: (2007)

To develop solid propellant based on kno3 with carbon mixture /
by: 184169 Mohd. Qayyam Omar, et al.
Published: (2008)

Fundamentals of solid-propellant combustion /
by: Kuo, Kenneth K., et al.
Published: (1984)

Design and fabrication of a 200N thrust rocket motor based on NH4CLO4 + Al solid propellant [electronic resource] /
by: Mastura Ab. Wahid, 1986-, et al.
Published: (2009)

Manufacturing large production quantities of precise solid propellant mixers/
by: 192504 Skovgard, Fred E., et al.
Published: (1965)

Development of pressurised burning rate test rig for solid propellant /
by: 428135 Nasrulhakim Musa, et al.
Published: (2007)

Development of a burning rate test rig for solid propellant [electronic resource] /
by: 454543 Intan Noryanah Kimsin
Published: (2007)

Performance of potassium nitrate as solid propellant /
by: Mohammad Nazri Mohd. Ja'afar, et al.
Published: (2002)

Development of a burning rate test rig for solid propellant /
by: 454543 Intan Noryanah Kimsin, et al.
Published: (2007)

Thermal and oxidative degradation mechanism of hydroxyl terminated natural rubber for solid rocket propellant binders
by: Baharulrazi, Norfhairna
Published: (2024)

A development of 500N thrust rocket motor using KNO3 carbon propellant [electronic resource] /
by: Amir Aziz, author, et al.
Published: (2008)

Solid propellant chemistry, combustion, and motor interior ballistics /
by: Yang, Vigor, et al.
Published: (2000)

Design and fabrication of a 200N thrust rocket motor based on NH4CLO4 + Al solid propellant /
by: Mastura Ab. Wahid, 1986-, et al.
Published: (2009)

A study of burning characteristic of AP68AL15HTPB17/13 propellant at atmosphere, 2 bar and 4 bar chamber pressure [electronic resource] /
by: Muhammad Aiman Talib, 1991-, et al.
Published: (2014)

Characteristic of potassium nitrate based solid rocket propellant /
by: Mohammad Nazri Mohd. Ja'afar, et al.
Published: (2002)

A study of burning characteristic of AP68AL15HTPB17/13 propellant at atmosphere, 2 bar and 4 bar chamber pressure /
by: Muhammad Aiman Talib, 1991-, author 637224, et al.
Published: (2014)

Development of crawford bomb time measuring instrumentation [electronic resource] /
by: Shahrul Ikhwan Abdul Khalid, 1985-
Published: (2009)

A development of 500N thrust rocket motor using KNO3 carbon propellant /
by: Amir Aziz, author, et al.
Published: (2008)

Membangunkan bahan dorong ammonium nitrat sebagai bahan dorong roket pepejal /
by: 387875 Shah Rizal Ruslan
Published: (2006)

Membangunkan bahan dorong ammonium nitrat sebagai bahan dorong roket pepejal [compact disc] /
by: 387875 Shah Rizal Ruslan
Published: (2006)

Development of crawford bomb time measuring instrumentation /
by: Shahrul Ikhwan Abdul Khalid, 1985-, et al.
Published: (2009)

Burning rate and characterization of hydroxyl terminated natural rubber/isophorone diisocyanate/glycerol propellant composites /
by: Juliana Jaafar, 1986-, et al.
Published: (2014)

Gas dynamics and thermodynamics of solid-propellant rockets/
by: 460055 Sorkin, R. E.
Published: (1969)

Development of rocket motor testing cradle [electronic resource] /
by: 487876 Adly Kalam
Published: (2008)

Solid rocket propulsion technology /
by: Davenas, Alain
Published: (1993)

Development of propellant binder using natural rubber [electronic resource] /
by: Khairul Muazam Shaharuddin, 1987-
Published: (2010)

Development of propellant binder using natural rubber /
by: Khairul Muazam Shaharuddin, 1987-, et al.
Published: (2010)

Development of rocket motor testing cradle/
by: 487876 Adly Kalam, et al.
Published: (2008)

Development of a rocket vehicle for weather modification /
by: 274137 Rizalman Mamat, et al.
Published: (2002)

Rekabentuk nozel untuk motor roket [electronic resource] /
by: 419069 Rafirul Hanif Ramli
Published: (2007)

Analysis of Thermal Decomposition of Solid Rocket Propellants
by: Marcin CEGŁA, et al.
Published: (2019-06-01)

Mereka bentuk propelan pepejal untuk roket kecil [electronic resource] /
by: 375369 Ahmad Saufi Mohamed Zahri
Published: (2006)

Propellant chemistry/
by: 295929 Sarner, Stanley F.
Published: (1966)

Pembangunan roket motor bersaiz kecil /
by: Mohammad Nazri Mohd. Jaafar, 1963-, et al.
Published: (2009)