Session
Technical Session VI: Support Systems
Abstract
Our goal is to design a 15,000 pound Small Launch Vehicle (SLV) which can carry a 250 kg payload into Low Earth Orbit (LEO). The objective is to develop a system to provide the SLV capability at a low cost. A preliminary analysis established for further refinement of the design. The SLV is a two state liquid oxygen/liquid hydrogen booster. Alternative fuels and engines are being investigated.
Small Launch Vehicle SS-88-35
Our goal is to design a 15,000 pound Small Launch Vehicle (SLV) which can carry a 250 kg payload into Low Earth Orbit (LEO). The objective is to develop a system to provide the SLV capability at a low cost. A preliminary analysis established for further refinement of the design. The SLV is a two state liquid oxygen/liquid hydrogen booster. Alternative fuels and engines are being investigated.
