Ongoing and completed research and development activities.
DTAP / DTAC
Differential Torque Actuated Propeller and Rotor Pitch Control. Up to date, a swashplate mechanism is the standard means...
Infusion Rigidizable Inflatable Space Elements. In the context of ASAP17 the consortium develops innovative, new...
Mars Aerobot Study
Rotating Wings Aerobot for the Martian Atmosphere. The objective of this study was the assessment of different rotary...
Lunar Tipjet Drone Concept
Rotating Tip Jet Drone for Lunar Surface Operations. We are introducing a drone for vacuum- and near-vacuum applications...
Venus Airship Concept
Rigid Partial Vacuum Airship for Venusian Atmosphere. The goal is to develop, manufacture, launch, deploy, transfer and...
Terrain Adaptive Landing Gear
Terrain Adaptive Landing Gear for a Lunar or Planetary Lander. We developed a very small packaged, deployable...
Inflatable Rgidizable Shelter or Habitat.
Development of inflatable and in-situ rigidizable composite structures for terrestrial- and space applications.
Galvanic Metal Matrix Composites combine the unique properties of carbon fibers, such as high specific tensile strength...
Lunar Lander Model
Full size lunar lander model for the german GXLP Team Part Time Scientists. The company was established in 2016, to...
Laser Sintered Fincan for High Power Rockets
Participating in the High Power Rocketry efforts at the TU Wien Sapceteam. We developed a one-piece internal isogrid...
Elliptic Lobe Cycloidal Pump
Development of an explicit expression for the parametric computation of cycloidal pump gears in the complex plane. This...
Electric Rocket Test Bed
Participating in the High Power Rocketry efforts at the TU Wien Sapceteam.
Lunar Lander Propulsion
Idendtification, defintion and classification of requirements for a propulsion system specification. Main driver was the...
GTO Ridshare Trans Lunar Injection
Harmonized requirements, trajectory design, simulation and optimization.
Lunar Orbit Insertion and Landing
Orbit insertion, circularization, optimized landing trajectory dessign and simulation.
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