GLOYER-TAYLOR LABORATORIES INC

Using modern additive manufacturing technology, GTL proposes to develop a geometry based thermal management system to enable the development of a Morphing Rocket Throat. With this capability, rocket m ...

In this effort GTL proposes to develop an additive production system for telescope mirrors leveraging previous research efforts for DARPA, MDA, and NASA. The proposed production method allows for a wi ...

In this phase I proposal GTL will leverage its experience in innovative composite tank design and production for spacecraft and propulsion systems in order to produce a high-performance composite torp ...

Ground based and airborne infrared astronomy is limited by atmosphere and telescope heat. These systems require a cold helium cooling of the instruments with a dewar for cryogen storage. Given the lim ...

In this phase I effort a design for a gas generation system architecture tailored for RCS gas accumulators on lander vehicles with ultra-low mass and thermal mass BHL components will be produced and P ...

Hypersonic vehicles and weapons systems offer the ability to quickly strike across the globe and are essential for the future of the U.S. armed forces. Operating these systems at hypersonic speeds pre ...

In this phase I effort ultra-light BHL composite transfer lines were shown to reduce chill-down time over 90% compared to equivalent stainless steel lines. BHL tubes have frac14; the mass of comparabl ...

GTLrsquo;s ultralightweight BHLtrade; dewar provides dramatically reduced mass, and increased performance over metal dewars. In cryogenic propellant storage systems, BHL has a demonstrated mass reduct ...

nbsp;For over 10 years GTL has been developing novel rocket system components. Originally funded by DARPA, with additional funding by NASA, GTL has developed a novel composite system (BHLtrade;) for c ...

In Situ Resource Utilization (ISRU) is at the forefront of near-term lunar and Martian missions.nbsp; While many technologies and program strategies focus in ISRU, propellant production substantially ...