NEW LAUNCH SYSTEMS

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

• 200 km circular orbit (LEO) à DV=7800 m/s

• 100 kg payload (nano and microsat’s)

• 3 stages:

– 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 )

• Numerical program developed to SIZE and DESIGN the whole vehicle (mass, geometry, dimensions) and to CALCULATE performance starting from missions requirements (Mach, Range, fuel, Istr)

• This code is able to size a broad range of  condition, from passengers transport  (SSTO) to launchers for missiles/small satellites (TSTO- avio launched)