The choice of structural materials for thermo thruster on clean monopropellant
Structural elements of a laboratory model of thermo engine on clean monopropellant are determined experimentally. The proposed elements and details incorporated into the design of a laboratory model.
1. Dyer J., Dinardi A., Anflo K. First Implementation of High Performance green propulsion in a constellation of small satellites // 27th Annual AIAA/USU Conference of Small Satellites. SSC13-VII-2.
2. Spores R. A., Masse R., Kimbrel S., McLean C. GRIM AF-M315E Propulsion System // 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA. P. 2013—3849.
3. Pokrupa N., Anflo K. Spacecraft system level design with regard to incorporation of a new green propulsion system // 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. AIAA. P. 2011—6129.