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
Engines
HyPER
2nd Stage
- Thrust 34 kN
- Burn Time 270 sec
- Specific Impluse 325 sec
- Propellant Paraffin / LOx
Propellant
Paraffin & Liquid Oxygen (LOx)
-
Affordability
Safer propellants cut safety infrastructure costs and lower launch service expenses.
-
Safety
Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.
-
Speed
Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.
Core Components
3D Printing Technology
-
Manufacturing core components of the HANBIT series engines with proprietary metal 3D printing technology.
-
Establishing a seamless, end-to-end process from development to mass production.
-
Enhancing launch service competitiveness through optimized quality, cost, and lead time.
Trajectory
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
Engines
LiMER
2nd Stage
- Thrust 29 kN
- Burn Time 300 sec
- Specific Impluse 350 sec
- Propellant Methane & LOx
Propellant
Paraffin & Liquid Oxygen (LOx)
-
Affordability
Safer propellants cut safety infrastructure costs and lower launch service expenses.
-
Safety
Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.
-
Speed
Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.
-
Efficiency
High specific impulse, re-ignitions, and precise thrust control ensure optimal performance for multi-launch missions.
-
Affordability
Methane fuel is easy to store and handle, leading to significant cost savings in operations.
-
Sustainability
Combustion minimizes environmental pollution, enabling more sustainable space launches.
Core Components
3D Printing Technology
-
Manufacturing core components of the HANBIT series engines with proprietary metal 3D printing technology.
-
Establishing a seamless, end-to-end process from development to mass production.
-
Enhancing launch service competitiveness through optimized quality, cost, and lead time.
Trajectory
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
Engines
LiMER
2nd Stage
- Thrust 29 kN x 2
- Burn Time 250 sec
- Specific Impluse 350 sec
- Propellant Methane & LOx
Engines
Kick Stage
- Thrust 4 kN
- Burn Time 390 sec
- Specific Impluse 350 sec
- Propellant Methane & LOx
Propellant
Paraffin & Liquid Oxygen (LOx)
-
Affordability
Safer propellants cut safety infrastructure costs and lower launch service expenses.
-
Safety
Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.
-
Speed
Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.
-
Efficiency
High specific impulse, re-ignitions, and precise thrust control ensure optimal performance for multi-launch missions.
-
Affordability
Methane fuel is easy to store and handle, leading to significant cost savings in operations.
-
Sustainability
Combustion minimizes environmental pollution, enabling more sustainable space launches.
Core Components
3D Printing Technology
-
Manufacturing core components of the HANBIT series engines with proprietary metal 3D printing technology.
-
Establishing a seamless, end-to-end process from development to mass production.
-
Enhancing launch service competitiveness through optimized quality, cost, and lead time.
Trajectory
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
Engines
HyPER
2nd Stage
- Thrust 245 kN
- Burn Time 150 sec
- Specific Impluse 325 sec
- Propellant Paraffin / Lox
Engines
LiMER
3rd Stage
- Thrust 29 kN x 2
- Burn Time 350 sec
- Specific Impluse 350 sec
- Propellant Methane & LOx
Propellant
Paraffin & Liquid Oxygen (LOx)
-
Affordability
Safer propellants cut safety infrastructure costs and lower launch service expenses.
-
Safety
Paraffin-based, non-toxic solid fuel minimizes the risk of explosion, ensuring exceptional safety and reliability.
-
Speed
Advanced fuel production innovations enable rapid manufacturing, significantly reducing launch lead times.
-
Efficiency
High specific impulse, re-ignitions, and precise thrust control ensure optimal performance for multi-launch missions.
-
Affordability
Methane fuel is easy to store and handle, leading to significant cost savings in operations.
-
Sustainability
Combustion minimizes environmental pollution, enabling more sustainable space launches.
Core Components
3D Printing Technology
-
Manufacturing core components of the HANBIT series engines with proprietary metal 3D printing technology.
-
Establishing a seamless, end-to-end process from development to mass production.
-
Enhancing launch service competitiveness through optimized quality, cost, and lead time.
Trajectory
