This inventor holds 3 USPTO granted patents and 1 EPO patent. Top assignee: The Boeing Company. Active years: 2019-2021.
Company Filing History:
Years Active: 2019-2021
Title: David S. Jenkins: Innovator in Rocket Propulsion Technology
Introduction
David S. Jenkins is a notable inventor based in Huntington Beach, CA (US). He has made significant contributions to the field of rocket propulsion technology, holding a total of 3 patents. His work focuses on enhancing the efficiency and safety of rocket fueling systems.
Latest Patents
One of Jenkins' latest patents is titled "Rocket propellant mixing and fueling systems and methods." This innovative rocket fueling system features an insulated jacket that can be removably coupled to a portion of a rocket, creating an enclosed space. The system includes a cryogen inlet designed to receive cryogen into the jacket's interior chamber, along with a cryogen outlet that provides the cryogen to the rocket. Additionally, it incorporates a gas outlet for exhausting cryogen and a flammable gas sensor to detect any flammable gases. Another significant patent is for "Methods, systems and apparatuses for combustible lead for high triple point propellants." This invention focuses on delivering high triple point propellant to a rocket engine while maintaining the desired phase during ignition.
Career Highlights
David S. Jenkins is currently employed at The Boeing Company, where he continues to develop cutting-edge technologies in aerospace. His expertise in rocket propulsion has positioned him as a key player in the industry.
Collaborations
Throughout his career, Jenkins has collaborated with talented individuals such as Daniel A. Watts and Albert D. Olsen. These partnerships have contributed to the advancement of innovative solutions in rocket technology.
Conclusion
David S. Jenkins is a prominent inventor whose work in rocket propulsion technology has led to significant advancements in the field. His patents reflect a commitment to improving rocket fueling systems and ensuring safety in aerospace applications.
