MMR-06

The MMR06 is a Soviet/Russian rocket for meteorological experiments, with a length of 3.48 metres and a total weight of 130 kg. The MMR06 rocket was built in two versions: One version had a conical top, the second one, named MMR06-M, had a detachable free flying top, also called dart. The maximum flight height was about 60 - 80 kilometres. Between 1988 and 1992 62 rockets of the type MMR06-M were launched from the former NVA exercise area Zingst, in order to accomplish wind and temperature measurements in the upper atmosphere.

==Technical data of MMR06-M== ===Total=== {| border="1" | Total mass || 134 ±5 kg |- | Mass empty || 58 kg |- | Fuel mass || 78 kg |- | Length || 4.14 m |- | colspan="2"|   |- | Distance from end of nozzle tocenter of gravity at launch || 1.445 m |- | Distance from end of nozzle tocenter of gravity at burn-out (Brennschluss) || 1.872 m |- | Distance from end of nozzle tocenter of wind pressure || 1 m |- | colspan="2"|   |- | Axial moment of inertia at launch || 0.87 kg/m2 |- | Axial moment of inertia at burn-out || 0.25 kg/m2 |- | colspan="2"|   |- | Equatorial moment of inertia at launch || 394.5 kg/m2 |- | Equatorial moment of inertia at burn-out || 158.5 kg/m2 |} {| align="right" |----- align="center" | schematic flight path of MMR06-M rocketschematic flight path of MMR06-M rocket |}