NEW LAUNCH SYSTEMS

SHAR has been designed with the motives of Simplicity, Re-Usability, and Sustainability for LEO orbits with a 

1st stage - Solid booster: 0 to 25 km and Mach 0 to 6

2nd stage - Scramjet: 25 to 50 km and Mach 6 to 10 [ Powered and shut-down flight phases ]

3rd stage - Hybrid rocket: 50 to 200 km ( Hohmann transfer to orbit )