columbus · Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source

Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source

Title: Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source
Date: 1962
Index Abstract: Coming Soon
Photo Quality: Undetermined
Report Number: AEDC TDR 62-15
Creator: Carman, C. T.
Corporate Author: Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Extent: 26
Identifier: AD0273488
Access Rights: Unknown
Distribution Classification: 1
Contract: AF 40(600)-800
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: None
Distribution Conflict: No
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.
Report Availability: Not available via Contrails
Date Issued: 1962-03
Publisher: Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force
Index In: DTIC
Type: report