mDraupner launch

µDraupner was designed with the single purpose of achieving supersonic flight within the range limitations of Rømø test range.

To accomplish this, it was nessecary to combine high mass ratio with small mass, short burning time and relatively large air drag. This was achieved by building µDraupner relatively small.

Project overview

Launch date 2005-09-05
Type Solid propellant rocket
Diameter ø60mm
Launch mass 2.04 kg
Propellant mass 0.82 kg
Maximum speed ~ Mach 1.8

More details are available at:

µDraupner - probably the first supersonic amatuer rocket in Denmark.