MMR06

The MMR06 is a Russian rocket for meteorological experiments. It is 3.48 meters long and has a launch weight of 130 kg. The MMR06 rocket was built in two versions: The first version had a conical tip, the second, also called MMR06 -M, a detachable free flight body ( Dart ). The peak heights are 60 and 80 kilometers. Between 1988 and 1992, 62 missiles MMR06 -M were started by former NVA training area on the peninsula Zingst to perform wind and temperature measurements in the upper atmosphere.

  • 2.1 ship
  • 2.2 country

Technical data of the MMR - 06M

Overall system rocket

  • Take off weight: 134 / - 5 kg
  • Mass: 58 kg
  • Fuel mass: 78 kg
  • Overall length: 4.14 m
  • Distance nozzle end - emphasis on startup: 1.445 m
  • Distance nozzle end - Focus at the end of firing: 1,872 m
  • Distance nozzle end - air raid point: 1m
  • Axial moment of inertia when starting: 0,87 kg / m²
  • Axial moment of inertia at the end of firing: 0.25 kg / m²
  • Equatorial inertial torque at start: 394.5 kg / m²
  • Equatorial moment of inertia at the end of firing: 158.5 kg / m²

Aerodynamic Coefficients

  • Cw = 0.42
  • Ca = 20
  • Cm = 34.4
  • Burnout velocity: 1428 m / s
  • Speed ​​of rotation of the missile about its own axis 800 revolutions / minute

Rocket motor

  • Mass loading: 121.8 kg
  • Mass with uncharged transition piece: 38 kg
  • Mass unloaded without transition piece: 33 kg
  • Length with transition piece: 2.813 m
  • Length without transition piece: 2.444 m
  • Burnout time: 7.2 to 12 s
  • Diameter: 0.2 m
  • Span with wings: 0.6 m
  • Incidence of the wing: 5-40 '

Darts

  • Mass: 12.2 kg
  • Length: 1,478 m
  • Diameter: 0.063 m
  • Distance Dartende - Focus: 0.78 m
  • Distance Dartende - Luftangrffspunkt: 0.5 m
  • Axial moment of inertia: 0.00752 kg / m
  • Equatorial inertia: 3,48 kg / m²
  • Wing span: 0.148 m
  • Angle of the blades to the longitudinal axis: 0 degrees
  • Speed ​​of ejection of the probe: 3.65 m / s
  • Aerodynamic coefficients:
  • Cw = 0.15
  • Ca = 20
  • Cm = 34.4

Parachute system

  • Mass 1 kg
  • Time of discharge 130s

Starting places

Ship

  • Musson
  • Ushakov

Country

  • Zingst peninsula, GDR
  • Kapustin Yar, Caspian Sea, Russia
  • Molodjoschnaja Station, Antarctica, Enderbyland
  • Geophysical Research Station E.T. Krenkel, Franz Joseph Land
  • Priliw
  • Volna
Dart (rocketry) List of rocket experiments on Zingst
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