Study of unusable liquid propellant residues evaporation processes parameters in the tanks of launch vehicle worked-off stage in microgravity

Study of unusable liquid propellant residues evaporation processes parameters in the tanks of launch vehicle worked-off stage in microgravity

A method is proposed for studying the evaporation process of unusable rocket propellant residues in worked-off stage under weightless conditions. Two options are considered as boundary conditions for liquid rocket propellant residues: a) liquid drop distribution in N identical drops, which surface...

Full description

Saved in:
Bibliographic Details
Main Authors: V. I. Trushlyakov, V. A. Urbansky
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2019-06-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Subjects:
worked-off rocket stage
liquid propellant residues
hydrogen peroxide
heat carrier
evaporation
Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2019/%D0%A2.%203,%20%E2%84%96%202%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/103-114%20%D0%A2%D1%80%D1%83%D1%88%D0%BB%D1%8F%D0%BA%D0%BE%D0%B2%20%D0%92.%20%D0%98.,%20%D0%A3%D1%80%D0%B1%D0%B0%D0%BD%D1%81%D0%BA%D0%B8%D0%B9%20%D0%92.%20%D0%90..pdf
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items

Similar Items