Rocket CMC-ZBX460 was launched on target area .The propellant is being re -experimented for a hi-grade extreme thruster which features are hybrid-a combination of a powerful fuel.
Objectives:
To develop a based hybrid fuel with less oxidant burner to simulate excellent propulsion.
Detail for a mini launch decoy rocket 3-5km with reconnaissance modules to log capsule recovery plus tele-sensing of confidential datum
Detail (1) Stages launching of hi-obtainable propellant.
Detail(2) Thermodynamic and Aerodynamic analysis of Rocket CMC-ZBX460
Analysis:
Fuel(A)
Fuel(B)
+Oxidizer
A+B +(O+)=ZBX460
Summary:
Conclusions:
