1940 - Instrumental in calculating thrust-to-weight ratio for engine performance
Mathematics
About This Innovation
* During her time at NASA Jet Propulsion Laboratory, Canright calculated thrust from rocket engines and analyzed the data to increase performance. * One of Canright's crowning achievements was the successful use of rockets for bomber aircraft. * After the successful development of jet propulsion bombers, her company JPL shifted its focus to designing a rocket which would reach a higher altitude than a helium-filled balloon. * Canright, along with Melba Nead, Virginia Prettyman, and Macie Roberts, were responsible for calculating the potential of rocket propellants. * In 1943, after the success of designing and testing of a rocket propellant, Canright became pregnant with her first child. Due to the unavailability of maternity leave in 1943, Canright had to resign.
The Invention
None
Key Information
Category:
Mathematics
Completion Status:
yes
Patent Number:
N/A
Co-Inventor:
None
Patent Information
Patent Number: N/A
Technical Specifications
N/A
Collaboration
Co-Inventor: None