Brigham City, UT, United States of America

C Max White

This inventor holds 4 USPTO granted patents. Top assignees: Thiokol Corporation, Morton Thiokol Inc.. Active years: 1985-1992.


% Patents Active = 100.0

Average Co-Inventor Count = 1.6

ph-index = 2

Forward Citations = 22(Granted Patents)


Company Filing History:


Years Active: 1985-1992

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4 patents (USPTO):Explore Patents

Title: C Max White: Innovator in Rocket Motor Technology

Introduction

C Max White is a notable inventor based in Brigham City, Utah, recognized for his contributions to rocket motor technology. He holds a total of 4 patents that showcase his innovative approach to igniter systems and propulsion mechanisms.

Latest Patents

One of his latest patents is the "Spherical igniter for full head-end web rocket motors." This invention features two molded urethane hemispherical shells lined with solid propellant fuel, forming a spherical pressure vessel. The design includes a fiberglass wrap for strength, an igniter initiator housed in a tubular urethane casing, and nozzle ports for gas discharge. Another significant patent is the "Radial pulse motor igniter-sustain grain." This invention involves a radial pulse rocket motor with hollow boost and sustain propellant grains, featuring a thermal barrier and a multiple pulse arm-fire device for precise ignition control.

Career Highlights

C Max White has worked with prominent companies in the aerospace sector, including Thiokol Corporation and Morton Thiokol Inc. His experience in these organizations has significantly influenced his innovative designs and patent developments.

Collaborations

Throughout his career, C Max White has collaborated with notable individuals such as Roger A Grosgebauer and James D Rozanski. These partnerships have contributed to the advancement of rocket motor technology and igniter systems.

Conclusion

C Max White's innovative work in rocket motor technology and his impressive patent portfolio highlight his significant contributions to the field. His inventions continue to influence advancements in aerospace engineering and propulsion systems.

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