Matbir rocket engine inc.
introducing the Mantis Rocket Engine™ gen 1.
The Mantis Rocket Engine™ is designed to work at its maximum efficiency in vacuum. With long and efficient burn times, a very high ∆v can be attained.
It's main fuel source is Cryogenic liquid hydrazine combined with Nitrogen tetroxide as oxidizer. With a mix ratio of 60:40.
Mantis engine fairing and cable network. Dry weight of 1478 kg without fairing.
