Bear, DE, United States of America

Robert G Gleeson


Average Co-Inventor Count = 3.4

ph-index = 2

Forward Citations = 26(Granted Patents)


Company Filing History:


Years Active: 1991-1993

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2 patents (USPTO):Explore Patents

Title: The Innovative Contributions of Robert G. Gleeson

Introduction

Robert G. Gleeson is a notable inventor based in Bear, Delaware, who has made significant contributions to the field of solid propellant rocket technology. With a total of 2 patents to his name, Gleeson's work focuses on enhancing the safety and efficiency of rocket motor cases.

Latest Patents

Gleeson's latest patents include a design for a solid propellant rocket motor case that meets insensitive munitions requirements. This innovative case is surrounded by a wrapping made of load-bearing material, which can withstand the hoop load during normal firing. The material is engineered to lose strength or melt at temperatures above normal storage levels but below the autoignition temperature of the propellant. This design allows for the safe venting of gases during undesired high storage temperatures, thereby preventing explosions. Another significant patent involves the use of diaminoglyoxime and diaminofurazan in solid propellants based on ammonium perchlorate, which improves the performance of these propellant compositions.

Career Highlights

Gleeson has spent a considerable part of his career at Thiokol Corporation, a leader in aerospace and defense technologies. His work has been instrumental in advancing the safety and effectiveness of rocket propulsion systems.

Collaborations

Throughout his career, Gleeson has collaborated with esteemed colleagues such as Frederick W. Van Name and Michael A. Gerace, contributing to a rich environment of innovation and development.

Conclusion

Robert G. Gleeson's contributions to rocket technology exemplify the importance of innovation in ensuring safety and performance in aerospace applications. His patents reflect a commitment to advancing the field and addressing critical challenges in propellant technology.

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