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HANBIT–Micro

HANBIT-Micro is a 2 stage smallsat launcher capable of carrying a 150kg payload to a 500km SSO orbit. The 1st stage employs a cluster of four 150kN thrust engines & the 2nd stage, a 60kN thrust engine. Both stages are powered by Hybrid rocket engines that use LOx / Paraffin based propellants and use an electric pump feed system.
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hanbit-m
n-m-payload
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Payload
Payload Mass
150 kg
Height
1.0 m
Diameter
1.5 m
  • payload01
  • payload02
n-m-payload
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2nd Stage
  • Height7.7 m
  • Diameter1.9 m
  • Thrust1 x max 60kN
  • Burn Time150 sec
  • Specific Impulse325 sec
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  • 2nd_02
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1st Stage
  • Height11.4 m
  • Diameter2.7 m
  • Thrust4 X 150kN
  • Burn Time150 sec
  • Specific Impulse292 sec
  • 1st_01
  • 1st_02
m-m-payload
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Payload
Payload Mass
150 kg
Height
1.0 m
Diameter
1.5 m
  • payload01
  • payload02
n-m-payload
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2nd Stage
  • Height7.7 m
  • Diameter1.9 m
  • Thrust1 x max 60kN
  • Burn Time150 sec
  • Specific Impulse325 sec
  • 2nd_01
  • 2nd_02
n-m-payload
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1st Stage
  • Height11.4 m
  • Diameter2.7 m
  • Thrust4 X 150kN
  • Burn Time150 sec
  • Specific Impulse292 sec
  • 1st_01
  • 1st_02

LAUNCH SITE & TRAJECTORY

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    LAUNCH SITES

    Alcantara Space Center, Brazil
    - 107° wide trajectory orbital inclinations
    - dialoguing with other launch sites to add to our launch site portfolio
    - capable of launch from anywhere on our portable launcher

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    Trajectory

    Launching from multiple launch sites, to provide a LOW-COST, LOW-LATENCY launch service to any orbital inclination