
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.

PROPELLANT -
RNX
THRUST -
31.305 kgf
VIDEO
MIRINAE IN FLIGHT

CANSAT
LAUNCH PROGRAM
Launch your satellite with Vega Space.