NASA CNTR
The hydrogen flow for the NASA Centrifugal Nuclear Thermal Rocket. The NASA CNTR concept is an innovative liquid-core nuclear rocket utilizing centrifugal forces for quick round trips to Mars with ~1500-1800s specific impulse and a 90-minute burn time.
NASA CNTR
The hydrogen flow for the NASA Centrifugal Nuclear Thermal Rocket. The NASA CNTR concept is an innovative liquid-core nuclear rocket utilizing centrifugal forces for quick round trips to Mars with ~1500-1800s specific impulse and a 90-minute burn time.
N/A
Under construction...
N/A
Under construction...
N/A
Under construction...
N/A
Under construction...
Get in touch with me at colavecchionick@gmail.com
Get in touch with me at colavecchionick@gmail.com
N/A
Under construction...
N/A
Under construction...
Formula SAE
Under construction...
Research
Undergraudate research assistant. Page under construction...
Nicholas Colavecchio
Mechanical engineering student at the University of Rhode Island.
NASA CNTR
The hydrogen flow for the NASA Centrifugal Nuclear Thermal Rocket. The NASA CNTR concept is an innovative liquid-core nuclear rocket utilizing centrifugal forces for quick round trips to Mars with ~1500-1800s specific impulse and a 90-minute burn time.