Specifications

Height- 12m
Diameter- 1.6m
Stages-2+kick stages
Wet Mass-14.257 Tonnes
Payload to LEO-200kg
Structure-Carbon Composite
Propellant-LOX/Paraffin

Overview

Our inaugural launch vehicle, Mayeen I, embodies the spirit of innovation and excellence that defines Voyager Mayeen. Designed with precision engineering and state-of-the-art technology, Mayeen-I is capable of reaching Low Earth Orbit(LEO) with an apogee of 500 km.

Specifications

Height- 12m
Diameter- 1.6m
Stages-2+kick stages
Wet Mass-14.257 Tonnes
Payload to LEO-200kg
Structure-Carbon Composite
Propellant-LOX/Paraffin

Overview

Our inaugural launch vehicle, Mayeen I, embodies the spirit of innovation and excellence that defines Voyager Mayeen. Designed with precision engineering and state-of-the-art technology, Mayeen-I is capable of reaching Low Earth Orbit(LEO) with an apogee of 500 km.

Specifications

Height- 12m
Diameter- 1.6m
Stages-2+kick stages
Wet Mass-14.257 Tonnes
Payload to LEO-200kg
Structure-Carbon Composite
Propellant-LOX/Paraffin

Overview

Our inaugural launch vehicle, Mayeen I, embodies the spirit of innovation and excellence that defines Voyager Mayeen. Designed with precision engineering and state-of-the-art technology, Mayeen-I is capable of reaching Low Earth Orbit(LEO) with an apogee of 500 km.

  • First Stage
  • Second stage
  • Kick Stage

Mayeen I engine has 3 Paglianti engines fully made up of carbon composites, from tanks to structure. First stage generates about 161KN thrust taking MAYEEN I upto 80km

  • Height: 6.57 m
  • Diameter: 1.6m
  • Number of Engines: 3
  • Burn time: 138s
  • Materials: Carbon Composites

2nd stage is powered by single Paglianti Vacuum Engine. Second engine takes 200 kg payload to desired orbit with required orbital velocity

  • Height: 3.93m
  • Diameter: 1.6m
  • Burn TIme: 240s
  • Number of Engines: 1
  • Materials: Carbon Composites

Kickstage had RCS system for upto 6dof control for precise payload orbit insertion. It dynamically adapts to diverse mission requirements and Pinpoint precision in payload deployment. Our Kick Stage will also convert into a satellite upon deployment of payloads.

  • First Stage
  • Second stage
  • Kick Stage

Mayeen I engine has 3 Paglianti engines fully made up of carbon composites, from tanks to structure. First stage generates about 161KN thrust taking MAYEEN I upto 80km.

  • Height: 6.75 m
  • Diameter: 1.6m
  • Number of Engines: 3
  • Burn time: 138s
  • Materials: Carbon Composites

2nd stage is powered by single Paglianti Vacuum Engine. Second engine takes 200 kg payload to desired orbit with required orbital velocity.

  • Height:3.93m
  • Diameter: 1.6m
  • Burn TIme: 240s
  • Number of Engines: 1
  • Materials: Carbon Composites

Kickstage had RCS system for upto 6dof control for precise payload orbit insertion. It dynamically adapts to diverse mission requirements and Pinpoint precision in payload deployment. Our Kick Stage will also convert into a satellite upon deployment of payloads.

  • First Stage
  • Second stage
  • Kick Stage

Mayeen I engine has 3 Paglianti engines fully made up of carbon composites, from tanks to structure. First stage generates about 161KN thrust taking MAYEEN I upto 80km.

  • Height: 6.57 m
  • Diameter: 1.6m
  • Number of Engines: 3
  • Burn time: 138s
  • Materials: Carbon Composites

2nd stage is powered by single Paglianti Vacuum Engine. Second engine takes 200 kg payload to desired orbit with required orbital velocity.

  • Height: 3.93m
  • Diameter: 1.6m
  • Burn TIme: 240s
  • Number of Engines: 1
  • Materials: Carbon Composites

Kickstage had RCS system for upto 6dof control for precise payload orbit insertion. It dynamically adapts to diverse mission requirements and Pinpoint precision in payload deployment

Paglianti Engine

Mayeen I is powered by 3 custom made Paglianti Engines which is an advanced hybrid propulsion system fully made in Nepal. Paglianti Engine uses Liquid oxygen as oxidizer and Paraffin wax as Fuel.

Specifications

ISP: 313s
Lift-off Thrust: 53.8 KN
Peak Thrust: 67KN
Cycle type: Turbopump fed
Propellant: Hybrid(LOx/Paaraffin wax)

Paglianti Engine

Mayeen I is powered by 3 custom made Paglianti Engines which is an advanced hybrid propulsion system fully made in Nepal. Paglianti Engine uses Liquid oxygen as oxidizer and Paraffin wax as Fuel.

Specifications

ISP: 313s
Lift-off Thrust: 53.8 KN
Peak Thrust: 67KN
Cycle type: Turbopump fed
Propellant: Hybrid(LOx/Paaraffin wax)

Paglianti Engine

Mayeen I is powered by 3 custom made Paglianti Engines which is an advanced hybrid propulsion system fully made in Nepal. Paglianti Engine uses Liquid oxygen as oxidizer and Paraffin wax as Fuel.

Specifications

ISP: 313s
Lift-off Thrust: 53.8 KN
Peak Thrust: 67KN
Cycle type: Turbopump fed
Propellant: Hybrid(LOx/Paaraffin wax)

Watch Mayeen 1 Flight Profile Animation

Watch Mayeen 1 Flight Profile Amination
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