Technical Paper
Silicon Based Fuels for Space Flight
2005-10-03
2005-01-3412
Limiting factors in air and space propulsion systems affect both design and operation of the engines and the energy derived from a fuel source. Translation of the fuel source to energy (combustion) always requires an oxidizer. The process of breaking the energy-laden bonds of the fuel has classically been achieved using the oxygen in air for air-breathing engines or an onboard source of oxidizer for spaceflight. This is a critical limitation for a possible single-stage vehicle, because the weight of the fuel and oxidizer needed to achieve the necessary speed and altitude for orbit is excessive. This problem was overcome using multi-stage engines that are discarded sequentially during vertical ascent. However, the relative inefficiency of fuels currently available perpetuates the requirement for multi-stage engines to achieve orbit. Multi-stage rockets still require onboard fuel and oxidizer at lift-off that can account for over 95% of the lift-off weight.