Рет қаралды 892
Current plan:
Designing to withstand ~Mach 1.5
~3Km altitude
APCP propellant(seems like I've to switch to dextrose or sorbitol based propllant to save time)
Custom machined rocket motor
Single deploy parachute
Non similar dual redundant flight computers
~1.3m tall(the open rocket design is older version)