Specifications
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
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
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
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
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.