Document Type : Research Paper

Authors

• Amirhossain Adami ¹
• zahra pourJabari ²
• Mohammad azhdari ²
• Ali Saadat dar ³
• Hanieh Eshaghnia ⁴
• Kazem gholipour ²
• seyedmohammad mirmohammadi ²
• Alireza Ahangarani Farahani ⁵

¹ Aerospace University Complex, Malik Ashtar University of TechnologyT Tehran, Iran

² Faculty of Aerospace Engineering, Malek Ashtar University of Technology

³ Malek Ashtar university of Technology

⁴ malek ashtar university of technology tehran

⁵ Malek-Ashtar University of Technology

Abstract

In this research, the structure of the probes sent to other planets is first investigated and the common structures are introduced. In the following, the system design process of the Armita probe, which was prepared for the first national competition of the probe robot (Iran Space Research Institute), will be discussed. Armita team has won the first place in the first phase of the competition in 1401. The probe design process is based on the ECSS standard and is presented briefly, which includes the compilation and extraction of the requirements document, function-performance tree, product tree and finally the conceptual design of the sub-systems to achieve the intended mission. Based on the extracted results, the Armita probe with a mass of 6.9 kg and geometric dimensions of 48 x 38 x 36 cm with a total energy consumption of 112 amp hours will be able to perform the intended mission and satisfy all technical, dimensional and mass requirements well. shows

Keywords

• Probe
• lunar rover
• system design
• ECSS standard
• product tree
• function tree
• conceptual design

Main Subjects

• Space systems design (spacecraft, satellites, space stations and their equipment)