A Hybrid-Electric Flying Wing as an Atmospheric Carrier of Launchers for Small Satellites Deployed in LEO

Recent years have seen a significant increase in the demand for and use of low earth orbit satellites, often for commercial purposes. This trend highlights the need to consider more adaptable and cost-effective launch systems. This paper presents the results of a conceptual investigation into the development of a low-cost 'carrier-launcher' configuration to facilitate Low Earth Orbit space missions. Based on a preliminary study, the integration of a hybrid-electric propulsion system and the adoption of a curved wing configuration for the flying wing are considered in this study. The carrier, a remotely piloted unmanned flying wing, is designed to serve as the first stage of a multi-stage rocket to launch payloads into Low Earth Orbit.