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.
|Type||Solid propellant rocket|
|Launch mass||2.04 kg|
|Propellant mass||0.82 kg|
|Maximum speed||~ Mach 1.8|
More details are available at: