1963NASA Technical Reports Server (NASA)Requires access

THE DEVELOPMENT OF A HEATED-HYBRID GENERATED GAS PRESSURIZATION SYSTEM FOR PROPELLANT TANKS

Daniel D. Evans, D. H. Lee

Open publisher page 0 citations

Abstract

Heated-hybrid generated gas pressurization system for liquid propellant transfer in rocket vehicles

About this research paper

What this paper is about

Heated-hybrid generated gas pressurization system for liquid propellant transfer in rocket vehicles

Why it matters

A significance statement is not available in the OpenAlex record.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Heated-hybrid generated gas pressurization system for liquid propellant transfer in rocket vehicles

Key concepts: Cabin pressurization, Propellant, Engineering, Environmental science, Petroleum engineering, Mechanical engineering, Aerospace engineering

Related papers

Back to paper searchBrowse research topicsOriginal source
THE DEVELOPMENT OF A HEATED-HYBRID GENERATED GAS PRESSURIZATION SYSTEM FOR PROPELLANT TANKS — Research Paper | ScholarLens