A new prototype of self-pressurizing fuel tank for micro and nano-satellites


Autoria(s): Cen, JW; Xu, JL
Data(s)

2009

Resumo

To increase effective load, light-weight micro-propulsion system is necessary for micro-satellites. Traditional propulsion systems including large and heavy high-pressure vessels are difficult to be scaled down to fulfill the demand of micro-satellites. In this article, a novel self-pressurizing fuel tank without high-pressure gas vessel is proposed. When some liquid propellant is consumed, pressure is compensated with CO2 released by heating NH4HCO3 powder in the fuel tank. Comparing with other types of self-pressurizing liquid fuel tank, a gas generator with special and simple structure was designed to stop or continue the NH4HCO3 decomposition reaction easily, and consumed a small amount of energy to heat the powder effectively. Performance tests showed that this new prototype is very suitable for micro-thrusters.

Identificador

http://ir.giec.ac.cn/handle/344007/3370

http://www.irgrid.ac.cn/handle/1471x/70289

Idioma(s)

英语

Fonte

Cen, JW; Xu, JL.A new prototype of self-pressurizing fuel tank for micro and nano-satellites,ACTA ASTRONAUTICA,2009,64(4):410-415

Palavras-Chave #Micro-propulsion system #Micro-satellite #Self-pressurizing #Liquid fuel tank
Tipo

期刊论文