Feasibility analysis of solar thermal propulsion system with thermal
Solar thermal propulsion (STP), which uses solar energy to heat propellant and can provide high specific impulse and thrust simultaneously, has been treated as promising alternative microsatellite propulsion techniques (Gerrish, 2016, Kennedy and Palmer, 2002, Leverone et al., 2019, Xing et al., 2013, Zhumaev and Shcheglov, 2019) mainly consists of