Editing MMR06 (section)

===Total===
{| border="1"
| Total mass || 134 ±5&nbsp;kg
|-
| Mass empty || 58&nbsp;kg
|-
| Fuel mass || 78&nbsp;kg
|-
| Length || 4.14 m
|-
| colspan="2"| &nbsp;
|-
| Distance from end of nozzle to<br />center of gravity at launch || 1.445 m
|-
| Distance from end of nozzle to<br />center of gravity at burn-out ([[Brennschluss]]) || 1.872 m
|-
| Distance from end of nozzle to<br />center of wind pressure || 1 m
|-
| colspan="2"| &nbsp;
|-
| Axial [[moment of inertia]] at launch || 0.87&nbsp;kg/m<sup>2</sup>
|-
| Axial moment of inertia at burn-out || 0.25&nbsp;kg/m<sup>2</sup>
|-
| colspan="2"| &nbsp;
|-
| Equatorial moment of inertia at launch || 394.5&nbsp;kg/m<sup>2</sup>
|-
| Equatorial moment of inertia at burn-out || 158.5&nbsp;kg/m<sup>2</sup>
|}
{| align="right"
|----- align="center"
| [[Image:MMR06-M flight path.png|schematic flight path of MMR06-M rocket]]<br /><small>schematic flight path of MMR06-M rocket</small>
|}