Journal of Space Science and Technology

Development of an Integrated Design Environment for Optimal Ascent Trajectory Planning

Pages 1-10

10.22034/jsst.2007.188402

S. Hossein Pourtakdost, M. Fakhri, Nima Asadian

• View Article
• PDF 359.59 K

Design of Attitude Control System of an Axisymmetric Satellite with Gravity Gradient Stabilization and Slow Spinning about Yaw Axis

Pages 11-19

H. Bolandi, B. Ghorbani Vaghei

• View Article
• PDF 474.31 K

Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters

Pages 21-36

M. Mirshams, H. Karimi, H. Naseh

• View Article
• PDF 596.07 K

Satellite Attitude Control by Magnetic Torquers with Variable Magnetic Intensity for Optimization of Power Consumption

Pages 37-45

M M. Moghaddam, A Salimi

• View Article
• PDF 703.88 K

Multidisciplinary Design Optimization of a Small Launch Vehicle; a System Sensitivity Analysis Approach

Pages 47-56

M. Ebrahimi, J. Jodey, J. Roshanian

• View Article
• PDF 414.26 K

Effects of Solar Activities, Drag Coefficient and Atmospheric Wind on Altitude Loss of a LEO Satellite

Pages 57-66

T. Abdollahi, A. Jahangirian, A. Naghash

• View Article
• PDF 722.98 K

Evaluation of the Effects of Radiation, Irradiance, and Temperature on Solar Cell Electrical Characteristics and Extraction of Maximum Solar Panel Power by MPPT

Pages 67-80

M. Taherbaneh, A.R. Fasooniehch, Sh. Karbasian, R. Amjadifard

• View Article
• PDF 687.95 K

Considerations of Utilizing Telemetry and GPS System in Sounding Rockets

Pages 81-86

B. Beheshti Boroumand, A. Ghanbarian, Z. Sadeghi Givi, A. Ahmadloo, K. Raissi, M. Bahrami

• View Article
• PDF 366.61 K