Testing of a Freeze-proof Condenser for the Tracker Thermal Control System on AMS-02
ICAS2016_0525: ENHANCING THE EXPLORATION OF AIRCRAFT CHANGEABILITY DURING CONCEPTUAL DESIGN
EXPERIMENTAL CHARACTERIZATION OF SUPERSONIC SPIN MOTOR NOZZLE FLOW
Surface UV Radiation Monitoring Based on GOME and SCIAMACHY (14)
Flight Mechanics Modeling of the PrandtlPlane for Conceptual and Preliminary Design
Das Verbesserungspotential von Systemen der Passiven Sicherheit für 50% Insassen
COMBINED AIRFRAME AND SUBSYSTEMS EVOLVABILITY EXPLORATION DURING CONCEPTUAL DESIGN