Analysis of the efficiency of hydrocarbon propellant cooling using liquid nitrogen and a combination of recuperative heat exchangers
Published: 11.03.2020
Authors: Aleksandrov A.A., Barmin I.V., Zolin A.V., Chugunkov V.V.
Published in issue: #3(99)/2020
DOI: 10.18698/2308-6033-2020-3-1965
Category: Aviation and Rocket-Space Engineering | Chapter: Ground Complexes, Launch Equipment, Aircraft Exploitation