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afterburning

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View High-temperature test facility at the NASA Lewis Engine Components Research Laboratory By Renato O. Colantonio

High-temperature test facility at the NASA Lewis Engine Components Research Laboratory

High-temperature test facility at the NASA Lewis Engine Components Research Laboratory

By Renato O. Colantonio

View Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine By Timothy R. Conners

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine

By Timothy R. Conners

View Advanced technology for aero gas turbine components By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Advanced technology for aero gas turbine components

Advanced technology for aero gas turbine components

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

View Combustion instabilities in liquid-fuelled propulsion systems By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Combustion instabilities in liquid-fuelled propulsion systems

Combustion instabilities in liquid-fuelled propulsion systems

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

View Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf By Milton Lamb

Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf

Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf

By Milton Lamb

View Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle By L. O. Brase

Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle

Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle

By L. O. Brase

View "2001: a space Odyssey" revisited--the feasibility of 24 hour commuter flights to the moon using NTR propulsion with LUNOX afterburners By Stanley K. Borowski

"2001: a space Odyssey" revisited--the feasibility of 24 hour commuter flights to the moon using NTR propulsion with LUNOX afterburners

"2001: a space Odyssey" revisited--the feasibility of 24 hour commuter flights to the moon using NTR propulsion with LUNOX afterburners

By Stanley K. Borowski

View Active chlorine and nitric oxide formation from chemical rocket plume afterburning By D. M. Leone

Active chlorine and nitric oxide formation from chemical rocket plume afterburning

Active chlorine and nitric oxide formation from chemical rocket plume afterburning

By D. M. Leone