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ReFEX
Das „Reusability Flight Experiment“ (ReFEx) ist ein Technologiedemonstrator für zukünftige geflügelte wiederverwendbare Stufen. Das Modell zeigt ReFEx in seiner Wiedereintrittskonfi guration, nachdem es von seiner Trägerrakete abgesetzt wurde
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Slush Propellants
Usually cryogenic propellants in launch vehicles are stored at the normal boiling point, but the density can be increased by subcooling the propellants.
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SpaceLiner
The SpaceLiner is an advanced, visionary concept for a suborbital, hypersonic, winged passenger transport, which is currently under investigation at DLR-SART. The two-stage vehicle will be powered by rocket propulsion.
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Expendable Launch Vehicle Concepts
The SART (Space Launcher Systems Analysis) group is responsible within DLR for the study and the development of new proposals for expendable launch vehicles.
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Supersonic and Hypersonic Transport
DLR-SART is actively involved in the definition and in preliminary design studies of advanced supersonic and hypersonic transport.
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Liquid Fly-back Booster (LFBB)
Current proposals for the introduction of reusable components in space transportation focus on winged fly-back boosters, powered by liquid rocket engines.
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