Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source
This citation is provided as a resource for researchers, but Contrails cannot provide a full-text download
U.S. government employees, Military/Department of Defense employees, and U.S. government contractors and sub-contractors may be eligible to register with the Defense Technical Information Center (DTIC), where this report and others like it may be available
Report Number: AEDC TDR 62-15
Author(s): Carman, C. T.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-03
Pages: 26
Contract: AF 40(600)-800
DoD Task:
Identifier: AD0273488
Abstract:
An Investigation Was Conducted To Determine The Feasibility Of Producing Large Quantities Of Gas As The Driving Medium Of Steam Ejectors By Directly Mixing Water With The Exhaust Gas Stream Of A Rocket-Type Combustion Chamber. The Feasibility Of Producing Large Quantities Of Steam-Gas Mixture Was Demonstrated. Gas With Specific Humidities Below The Saturated Value Was More Suitable As An Ejector Driving Fluid Than Saturated Mixtures. He Evaporative Efficiency Of The Rocket Steam Generating Rig Was In The Range From 91 To 103 Percent.
Author(s): Carman, C. T.
Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-03
Pages: 26
Contract: AF 40(600)-800
DoD Task:
Identifier: AD0273488
Abstract:
An Investigation Was Conducted To Determine The Feasibility Of Producing Large Quantities Of Gas As The Driving Medium Of Steam Ejectors By Directly Mixing Water With The Exhaust Gas Stream Of A Rocket-Type Combustion Chamber. The Feasibility Of Producing Large Quantities Of Steam-Gas Mixture Was Demonstrated. Gas With Specific Humidities Below The Saturated Value Was More Suitable As An Ejector Driving Fluid Than Saturated Mixtures. He Evaporative Efficiency Of The Rocket Steam Generating Rig Was In The Range From 91 To 103 Percent.