Abbasi-Moghadam, D. هدایت بهینه بر خط بازگشت به زمین از طریق بسط مجانبی هماهنگ [Volume 3, Issue 2, 2011, Pages 69-76]
Adami-Dehkordi, A. h. Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite [Volume 3, Issue 2, 2011, Pages 11-22]
Ahangar, M. An Investigation on the Effect of Chemical Kinetics Mechanisms in the Modeling of Combustive Gaseous Oxidizer Flow on a Solid Fuel Surface [Volume 3, Issue 1, 2010, Pages 1-13]
Amani, E. کاربرد مدل پاندول ساده به منظور اعمال دینامیک تلاطم سیال در شبیهسازی شش درجه آزادی پرواز ماهوارهبر [Volume 3, Issue 2, 2011, Pages 59-67]
Anbarloi, M. Design and Manufacturing a Laboratory Example of Pulsed Plasma Thruster [Volume 3, Issue 2, 2011, Pages 23-30]
Ariaii-Far, N. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]
B
Bahrami, M. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]
Baradaran Shokouhi, Sh. A Spin Satellite Imaging System Design with Real Time Imaging Capability Using FPGA [Volume 3, Issue 1, 2010, Pages 45-54]
Bazrafshan, H. A Spin Satellite Imaging System Design with Real Time Imaging Capability Using FPGA [Volume 3, Issue 1, 2010, Pages 45-54]
E
Ebrahimi, M. کاربرد مدل پاندول ساده به منظور اعمال دینامیک تلاطم سیال در شبیهسازی شش درجه آزادی پرواز ماهوارهبر [Volume 3, Issue 2, 2011, Pages 59-67]
Ebrahimi, R. An Investigation on the Effect of Chemical Kinetics Mechanisms in the Modeling of Combustive Gaseous Oxidizer Flow on a Solid Fuel Surface [Volume 3, Issue 1, 2010, Pages 1-13]
F
Farshchi, M. Design and Manufacturing a Laboratory Example of Pulsed Plasma Thruster [Volume 3, Issue 2, 2011, Pages 23-30]
Farsi, M. A. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]
G
Ghaderi-Dehkordi, Y. Investigation of the Effect of Reinforcement on Thermo-Physical Properties of Ablative Heat Shields [Volume 3, Issue 1, 2010, Pages 55-65]
Ghorbani Vagheii, B. A Spin Satellite Imaging System Design with Real Time Imaging Capability Using FPGA [Volume 3, Issue 1, 2010, Pages 45-54]
J
Jafari Nadoushan, M. Modeling Halo Orbits and the Associated Manifolds in the Restricted Three Body Problem [Volume 3, Issue 1, 2010, Pages 75-80]
Jafari Nadoushan, M. Studying of Effect of Regularization and Change of Independent Variable on the Solution of Perturbed 2BP [Volume 3, Issue 2, 2011, Pages 53-58]
Jalali Chimeh, S. A. R. Dynamic Simulation of Propellant Utilization System in Propellant Tanks of a Liquid Propellant Engine [Volume 3, Issue 2, 2011, Pages 31-43]
K
Kalantari-Nezhad, R. Investigation and Analysis of Seperation System of Kavoshgar-3 [Volume 3, Issue 1, 2010, Pages 15-23]
Karimi, H. Dynamic Simulation of Propellant Utilization System in Propellant Tanks of a Liquid Propellant Engine [Volume 3, Issue 2, 2011, Pages 31-43]
Khaladjzadeh, L. Drivation of System Level Characteristics of a Manned Spacecraft by Applying Statistics Models [Volume 3, Issue 1, 2010, Pages 25-36]
M
Marzban, Sh. A Method for Performance Enhancement for Aeronautical Telemetry Radio Link Using Alamouti Code [Volume 3, Issue 2, 2011, Pages 1-9]
Mirshams, M. Drivation of System Level Characteristics of a Manned Spacecraft by Applying Statistics Models [Volume 3, Issue 1, 2010, Pages 25-36]
Mohamed-Pour, K. A Method for Performance Enhancement for Aeronautical Telemetry Radio Link Using Alamouti Code [Volume 3, Issue 2, 2011, Pages 1-9]
Mohammadzaman, E. Short Time Stability Approach to Guidance Law Design [Volume 3, Issue 1, 2010, Pages 37-44]
Momeni, H. R. Short Time Stability Approach to Guidance Law Design [Volume 3, Issue 1, 2010, Pages 37-44]
Mortazavi, M. هدایت بهینه بر خط بازگشت به زمین از طریق بسط مجانبی هماهنگ [Volume 3, Issue 2, 2011, Pages 69-76]
N
Naderi Tabrizi, M. Dynamic Simulation of Propellant Utilization System in Propellant Tanks of a Liquid Propellant Engine [Volume 3, Issue 2, 2011, Pages 31-43]
Nasiri, N. Modeling and Simulating the Earth’s Magnetic Field Utilizing the 10th Generation of IGRF and Comparison the Linear and Nonlinear Transformation in order to Use in Satellite Attitude Control [Volume 3, Issue 2, 2011, Pages 45-52]
Navabi, M. Optimal Impulsive Maneuver Between Elliptical Coplanar-Noncoaxial Orbits [Volume 3, Issue 1, 2010, Pages 67-74]
Navabi, M. Modeling and Simulating the Earth’s Magnetic Field Utilizing the 10th Generation of IGRF and Comparison the Linear and Nonlinear Transformation in order to Use in Satellite Attitude Control [Volume 3, Issue 2, 2011, Pages 45-52]
Nosratollahi, M. Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite [Volume 3, Issue 2, 2011, Pages 11-22]
P
Pourtakdoust, S. H. Modeling Halo Orbits and the Associated Manifolds in the Restricted Three Body Problem [Volume 3, Issue 1, 2010, Pages 75-80]
R
Rezaiha, A. Design and Manufacturing a Laboratory Example of Pulsed Plasma Thruster [Volume 3, Issue 2, 2011, Pages 23-30]
Roshanian, J. کاربرد مدل پاندول ساده به منظور اعمال دینامیک تلاطم سیال در شبیهسازی شش درجه آزادی پرواز ماهوارهبر [Volume 3, Issue 2, 2011, Pages 59-67]
S
Sabatifar, M. Optimal Impulsive Maneuver Between Elliptical Coplanar-Noncoaxial Orbits [Volume 3, Issue 1, 2010, Pages 67-74]
T
Tivay, M. Studying of Effect of Regularization and Change of Independent Variable on the Solution of Perturbed 2BP [Volume 3, Issue 2, 2011, Pages 53-58]
