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SBIR/STTR

Turbopump Design for Deep Throttling Capability, Phase II

Completed Technology Project

Project Introduction

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 »

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A final report document may be available for this project. If you would like to request it, please contact us.

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