NASA-LLIS-0750

Lessons Learned – High Performance Liquid Hydrogen Turbopumps

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:19:42Z
date available	2017-09-04T15:19:42Z
date copyright	04/04/2000
date issued	2000
identifier other	MUCEQCAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/19548
description abstract	Practice: Understanding and addressing the design environment, component interactions, and potential failure modes are the keys to high reliability in high performance liquid hydrogen turbopumps for launch vehicle engines. Designing and using a combination of unique sealing, cooling, processing, material selection, and balancing techniques in response to engine design requirements will permit the development, production, and reliable flights of hydrogen turbopumps.
language	English
title	NASA-LLIS-0750	num
title	Lessons Learned – High Performance Liquid Hydrogen Turbopumps	en
type	standard
page	5
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;2000
contenttype	fulltext