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HANBIT

HANBIT is a hybrid-based orbital launch vehicle
designed to provide low-cost, rapid launch solutions.

OVERVIEW

  • Height 21.7 m
  • Diameter 1.4 m
  • Orbit ~500 km (SSO)
  • Payload 90 kg*

* Based on launching from the Alcântara Space Center

Engines

HyPER

1st Stage

  • Thrust 245 kN
  • Burn Time 150 sec
  • Specific Impluse 292 sec
  • Propellant Paraffin / LOx
제품이미지

Engines

HyPER

2nd Stage

  • Thrust 34 kN
  • Burn Time 270 sec
  • Specific Impluse 325 sec
  • Propellant Paraffin / LOx
제품이미지

Propellant

Paraffin & Liquid Oxygen (LOx)

  • Affordability Affordability

    Affordability

    Safer propellants cut safety infrastructure costs and lower launch service expenses.

  • Safety Safety

    Safety

    Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.

  • Speed Speed

    Speed

    Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.

Trajectory

발사궤적이미지

OVERVIEW

  • Height 21.8 m
  • Diameter 1.4 m
  • Orbit ~500 km (SSO)
  • Payload 90 kg*

* Based on launching from the Alcântara Space Center

Engines

HyPER

1st Stage

  • Thrust 245 kN
  • Burn Time 150 sec
  • Specific Impluse 292 sec
  • Propellant Paraffin / LOx
제품이미지

Engines

LiMER

2nd Stage

  • Thrust 29 kN
  • Burn Time 300 sec
  • Specific Impluse 350 sec
  • Propellant Methane & LOx
제품이미지

Propellant

Paraffin & Liquid Oxygen (LOx)

  • Affordability Affordability

    Affordability

    Safer propellants cut safety infrastructure costs and lower launch service expenses.

  • 안전성 안전성

    Safety

    Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.

  • Speed Speed

    Speed

    Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.

  • Efficiency Efficiency

    Efficiency

    High specific impulse, re-ignitions, and precise thrust control ensure optimal performance for multi-launch missions.

  • Affordability Affordability

    Affordability

    Methane fuel is easy to store and handle, leading to significant cost savings in operations.

  • Sustainability Sustainability

    Sustainability

    Combustion minimizes environmental pollution, enabling more sustainable space launches.

Trajectory

발사궤적이미지

OVERVIEW

  • Height 22.5 m
  • Diameter 1.4 m
  • Orbit ~500 km (SSO)
  • Payload 170 kg*

* Based on launching from the Alcântara Space Center

Engines

HyPER

1st Stage

  • Thrust 245 kN
  • Burn Time 130 sec
  • Specific Impluse 292 sec
  • Propellant Paraffin / Lox
제품이미지

Engines

LiMER

2nd Stage

  • Thrust 29 kN x 2
  • Burn Time 250 sec
  • Specific Impluse 350 sec
  • Propellant Methane & LOx
제품이미지

Engines

Kick Stage

  • Thrust 4 kN
  • Burn Time 390 sec
  • Specific Impluse 350 sec
  • Propellant Methane & LOx
제품이미지

Propellant

Paraffin & Liquid Oxygen (LOx)

  • Affordability Affordability

    Affordability

    Safer propellants cut safety infrastructure costs and lower launch service expenses.

  • Safety Safety

    Safety

    Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.

  • Speed Speed

    Speed

    Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.

  • Efficiency Efficiency

    Efficiency

    High specific impulse, re-ignitions, and precise thrust control ensure optimal performance for multi-launch missions.

  • Affordability Affordability

    Affordability

    Methane fuel is easy to store and handle, leading to significant cost savings in operations.

  • Sustainability Sustainability

    Sustainability

    Combustion minimizes environmental pollution, enabling more sustainable space launches.

Trajectory

발사궤적이미지

OVERVIEW

  • Height 39.6 m
  • Diameter 3.7 m
  • Orbit ~500 km (SSO)
  • Payload 1,300 kg*

* Based on launching from the Alcântara Space Center

Engines

HyPER

1st Stage

  • Thrust 245 kN x 9ea
  • Burn Time 130 sec
  • Specific Impluse 292 sec
  • Propellant Paraffin / Lox
제품이미지

Engines

HyPER

2nd Stage

  • Thrust 245 kN
  • Burn Time 150 sec
  • Specific Impluse 325 sec
  • Propellant Paraffin / Lox
제품이미지

Engines

LiMER

3rd Stage

  • Thrust 29 kN x 2
  • Burn Time 350 sec
  • Specific Impluse 350 sec
  • Propellant Methane & LOx
제품이미지

Propellant

Paraffin & Liquid Oxygen (LOx)

  • Affordability Affordability

    Affordability

    Safer propellants cut safety infrastructure costs and lower launch service expenses.

  • Safety Safety

    Safety

    Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.

  • Speed Speed

    Speed

    Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.

  • Efficiency Efficiency

    Efficiency

    High specific impulse, re-ignitions, and precise thrust control ensure optimal performance for multi-launch missions.

  • Affordability Affordability

    Affordability

    Methane fuel is easy to store and handle, leading to significant cost savings in operations.

  • Sustainability Sustainability

    Sustainability

    Combustion minimizes environmental pollution, enabling more sustainable space launches.

Trajectory

발사궤적이미지