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MIRINAE

 

LOW ALTITUDE CLASS ROCKET CAPABLE OF REFLIGHT

1

TOTAL LAUNCHES

0

TOTAL LANDINGS

0

REFLOWN ROCKETS

MIRINAE

 

OVERVIEW

 

Mirinae is a reusable, single-stage rocket developed and constructed by Vega Space in cooperation with Vega Propulsion Laboratory for the reliable transportation of payloads up to varying altitudes. 

In accordance with the theme of reusability, Mirinae is operated via processing software that enables the full-automation of parachute ejection process and landing leg deployment. 

HEIGHT - 

1.5M

DIAMETER - 

7.4cm

MASS - 

2.5kg

MAX ALTITUDE - 

1.0KM

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ENGINE

MIR

 

Mir is a solid propellant rocket engine developed by Vega Propulsion Laboratory for the Mirinae launch vehicle. Mir engine uses a RNX epoxy-based composite propellant and can produce over 30kg of thrust.
 

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PROPELLANT - 

RNX

THRUST - 

31.305 kgf

VIDEO

MIRINAE IN FLIGHT

Image by NASA

CANSAT 
LAUNCH PROGRAM

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Fullride Launch Option is a launch option that grants all of the launch and the operation of the satellite to Vega Space. Most of our customers choose this option, if they are not able to come down to the launch site, located in Jeju, South Korea.

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Semi-Ride Launch Option is a launch option that grants only the launch-related operation without the ability to test or operate the satellites. Our customers choose this option, if their team are able to come down to our launch site, located in Jeju, South Korea. 

Choose your Launch Option

Launch your satellite with Vega Space.