In the Spring of 2002, Aerojet experienced a major failure during a qualification test of the solid rocket motor that they were developing for the Atlas V Enhanced Expendable Launch Vehicle. In that test, hot combustion gas reached the O-rings in the nozzle-to-case joint and caused a structural failure that resulted in loss of the nozzle and aft dome sections of the motor. To improve the design of this joint, Aerojet decided to incorporate three braided carbon-fiber thermal barriers developed at the NASA Glenn Research Center. The thermal barriers were used to block the searing-hot 5500 F pressurized gases from reaching the temperature-sensitive O-rings that seal the joint. Glenn originally developed the thermal barriers for the nozzle join...
The NASA Glenn Research Center is developing advanced control surface seals and propulsion system se...
A complete run log of all tests conducted in the NASA-MSFC hot gas test facility during the developm...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
The Space Shuttle solid rocket motor case assembly joints are sealed using conventional 0-ring seals...
Assembly joints of modern solid-rocket motor cases are usually sealed with conventional O-ring seals...
The assembly joints of modem solid rocket motor cases are generally sealed using conventional O-ring...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
The evolution of the orbiter aft heat shield seal (AHSS) design, which involved advancing mechanical...
This presentation was part of the session : Sample Return ChallengesSixth International Planetary Pr...
NASA astronaut Scott Parazynski led the development of materials and techniques for the inspection a...
The major material and design challenges associated with the orbiter thermal protection system (TPS)...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
The National Aeronautics and Space Administration has undertaken a project to restore full-scale the...
For 6 years prior to the retirement of the Space Shuttle Program, the shuttles carried an onboard re...
NASA's Space Launch System (SLS) uses four clustered liquid rocket engines along with two solid rock...
The NASA Glenn Research Center is developing advanced control surface seals and propulsion system se...
A complete run log of all tests conducted in the NASA-MSFC hot gas test facility during the developm...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...
The Space Shuttle solid rocket motor case assembly joints are sealed using conventional 0-ring seals...
Assembly joints of modern solid-rocket motor cases are usually sealed with conventional O-ring seals...
The assembly joints of modem solid rocket motor cases are generally sealed using conventional O-ring...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
The evolution of the orbiter aft heat shield seal (AHSS) design, which involved advancing mechanical...
This presentation was part of the session : Sample Return ChallengesSixth International Planetary Pr...
NASA astronaut Scott Parazynski led the development of materials and techniques for the inspection a...
The major material and design challenges associated with the orbiter thermal protection system (TPS)...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
The National Aeronautics and Space Administration has undertaken a project to restore full-scale the...
For 6 years prior to the retirement of the Space Shuttle Program, the shuttles carried an onboard re...
NASA's Space Launch System (SLS) uses four clustered liquid rocket engines along with two solid rock...
The NASA Glenn Research Center is developing advanced control surface seals and propulsion system se...
A complete run log of all tests conducted in the NASA-MSFC hot gas test facility during the developm...
NASA sponsored the Turbine Engine Hot Section Technology (HOST) Project to address the need for impr...