Skip Navigation
Small Business Innovation Research/Small Business Tech Transfer

Turbopump Design for Deep Throttling Capability, Phase II

Completed Technology Project
529 views

Project Description

Turbopump Design for Deep Throttling Capability, Phase II
This project will demonstrate the benefits of a partial emission pump coupled with a zero net positive suction pressure inducer design to achieve robust, deep throttling capability. This pump application is well suited for 5k to 15k lbf thrust range rocket engines. More »

Anticipated Benefits

Primary U.S. Work Locations and Key Partners

Technology Transitions

Light bulb

Suggest an Edit

Recommend changes and additions to this project record.
^