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VOL_16_N_5
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Table of Contents
Articles
| Development of a Brute Force Method to Solve for Static and Dynamic Constrained Attitude Maneuver |
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| Ahmad Bataineh, Ahmad Fares, Ahmad Bani Younes, Wafa Batayneh | 189-197 |
| Drag Analysis on Rocket Nose Cones for Enhanced Flight Range |
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| Ahmad Riyadl, Idris Eko Putro, Rahmat Alfi Duhri, Oka Sudiana, Hakiki Hakiki, Azizul Hanif, Bagus Hayatul Jihad, Rika Andiarti | 198-206 |
| Optimizing Supersonic Rocket Efficiency: a Numerical Analysis of Aerodynamic Characteristics and Angle of Canard Deflection |
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| Mahdi Goucem, Raouf Khiri | 207-214 |
| Polymer Foam Materials for Vibration Damping in the Design and Development of the Mobile Thermal Vacuum Test Facility Prototype |
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| Sergey Kravchenko, Nikolay Kuleshov, Ilmars Blumbergs, Natalia Kravchenko, Vladimir Shestakov, Daria Panova, Nikolajs Glizde | 215-221 |
Erratum
| Design Contributions to the Attitude Control System of a Geostationary Satellite |
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| Abdelghani Guettat, Nabil Boughanmi | 222 |
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