This paper reports results of an investigation into developing a single failure tolerant pyrotechnic linear separation system which features completely redundant explosive trains suitable for human spaceflight. It is a follow up to Flat-H Redundant Frangible Joint Design Evolution 2017 and Flat-H Redundant Frangible Joint Evolution. The paper chronicles the history of the redundant frangible joint development program including testing, analysis, and design improvements from 2014 to the present culminating in a successful proof-of-concept prototype. The paper describes work done to address debris control and containment of combustion products. A performance optimization strategy is presented along with optimization results. Additionally a no...
In support of a stall/spin research program, an emergency in-flight egress system is being installed...
Following the failure of a previously qualified pyrotechnically actuated pin puller design, an inves...
Controlling the level of contamination for sensitive spacecraft instruments during launch and fairin...
Space vehicle staging and separation events require pyrotechnic devices. They are single-use mechani...
Orion and Commercial Crew Program (CCP) Partners have chosen to use frangible joints for certain sep...
Controlling the level of contamination for sensitive spacecraft instruments during launch and fairin...
This paper presents the methods by which NASA has designed, built, tested, and certified pyrotechnic...
An investigation to determine the most likely cause of two failures of five tests on 79 inch diamete...
Pyrotechnic shaped charge aerospace vehicle stage and shroud separation systems developmen
Following several flight and ground test failures of spacecraft systems using single-shot, 'normally...
During the initial certification test of the forward structural attachment of the space shuttle orbi...
Following several flight and ground test failures of spacecraft systems using single-shot, 'normally...
The application of pyrotechnics to aerospace systems has been resisted because normal engineering me...
Marshall Space Flight Center (MSFC) has developed a valve concept to replace traditional pyrotechnic...
The recently introduced discipline of Design for Demise aims to promote the atmospheric demise of a ...
In support of a stall/spin research program, an emergency in-flight egress system is being installed...
Following the failure of a previously qualified pyrotechnically actuated pin puller design, an inves...
Controlling the level of contamination for sensitive spacecraft instruments during launch and fairin...
Space vehicle staging and separation events require pyrotechnic devices. They are single-use mechani...
Orion and Commercial Crew Program (CCP) Partners have chosen to use frangible joints for certain sep...
Controlling the level of contamination for sensitive spacecraft instruments during launch and fairin...
This paper presents the methods by which NASA has designed, built, tested, and certified pyrotechnic...
An investigation to determine the most likely cause of two failures of five tests on 79 inch diamete...
Pyrotechnic shaped charge aerospace vehicle stage and shroud separation systems developmen
Following several flight and ground test failures of spacecraft systems using single-shot, 'normally...
During the initial certification test of the forward structural attachment of the space shuttle orbi...
Following several flight and ground test failures of spacecraft systems using single-shot, 'normally...
The application of pyrotechnics to aerospace systems has been resisted because normal engineering me...
Marshall Space Flight Center (MSFC) has developed a valve concept to replace traditional pyrotechnic...
The recently introduced discipline of Design for Demise aims to promote the atmospheric demise of a ...
In support of a stall/spin research program, an emergency in-flight egress system is being installed...
Following the failure of a previously qualified pyrotechnically actuated pin puller design, an inves...
Controlling the level of contamination for sensitive spacecraft instruments during launch and fairin...