Application of trioxygen difluoride in liquid- rocket-propellant technology.
Trioxygen difluoride additive rendering LOX hypergolic, discussing environmental limits of reliable hypergolic ignition with liquid and gaseous hydrogen
Amster, A. B.↗
Engineering topics
Capener, E. L.
Publications and source records attributed to Capener, E. L..
Application of trioxygen difluoride in liquid rocket propellant technology.
Trioxygen difluoride additive rendering LOX hypergolic, discussing environmental limits of reliable hypergolic ignition with liquid and gaseous hydrogen
Amster, A. B.↗
Propellant combustion phenomena during rapid depressurization Final report
Idealized combustion model in which exothermic or endothermic reactions are permitted at or very near solid-gas interfaces
Capener, E. L.↗
Evaluation of ozone difluoride as a liquid propellant additive Final report
Ozone difluoride evaluated as liquid propellant additive
PROPELLANT ADDITIVE↗
Studies on ionization phenomena associated with solid-propellant rockets.
Microwave attenuation magnitude associated with exhaust plasma of nonaluminized and aluminized composite propellant
COMPOSITE PROPELLANT↗
Propellant combustion phenomenon during rapid depressurization Quarterly report no. 1, Jul. 1 - Sep. 30, 1965
Theoretical studies of processes occurring during rapid depressurization of burning solid propellants
PROPELLANT COMBUSTION↗
Studies on ionization phenomena associated with solid propellant rockets.
Solid propellant composition and rocket motor design effect on plasma microwave and visible light attenuation emitted by exhaust
COMPOSITE PROPELLANT↗