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HANBIT–Mini

HANBIT-Mini is a 3 stage smallsat launcher capable of carrying a 500kg payload to a 500km SSO orbit. The 1st stage employs a cluster of seven 150kN thrust engines, the 2nd stage, a cluster of four 150kN thrust engines & the 3rd stages a single 60kN thrust engine. All stages are powered by Hybrid rocket engines that use LOx / Paraffin based propellants and use an electric pump feed system.
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n-m-payload
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Payload
Payload Mass
500 kg
Height
6.5 m
Diameter
2.3 m
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  • payload01
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3rd Stage
  • Height7.9 m
  • Diameter2.6 m
  • Thrust1 x max 60kN
  • Burn Time200 sec
  • Specific Impulse328 sec
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  • 3rd_02
n-m-payload
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2nd Stage
  • Height9.3 m
  • Diameter2.6 m
  • Thrust4 x max 150kN
  • Burn Time100 sec
  • Specific Impulse310 sec
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  • 2nd_02
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1st Stage
  • Height12.4 m
  • Diameter3.3 m
  • Thrust7 x 150kN
  • Burn Time100 sec
  • Specific Impulse292 sec
  • 1st_01
  • 1st_02
m-s-payload
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Payload
Payload Mass
500kg
Height
6.5 m
Diameter
2.3 m
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  • payload01
m-s-payload
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3rd Stage
  • Height7.9 m
  • Diameter2.6 m
  • Thrust1 x max 60kN
  • Burn Time200 sec
  • Specific Impulse328 sec
  • 3rd_01
  • 3rd_02
m-s-payload
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2nd Stage
  • Height9.3 m
  • Diameter2.6 m
  • Thrust4 x max 150kN
  • Burn Time100 sec
  • Specific Impulse310 sec
  • 2nd_01
  • 2nd_02
m-m-payload
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1st Stage
  • Height12.4 m
  • Diameter3.3 m
  • Thrust7 x 150kN
  • Burn Time100 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