Transient Burning of Hybrid Fuels in a Lab-scale Burner by an Optical Technique(Abstract)

摘要

Hybrid Rocket Engines (HREs) offer possible advantages over Solid Rocket Motors (SRMs) and Liquid Rocket Engines (LREs) such as thrust throttling and possible multiple ignitions. Considering the high safety and reliability of HREs, these attractive features could respond to novel and urgent operating applications such as active de-orbiting of satellites and spacecraft, and soft-landing systems.