Enhancing the efficiency of the propellant cooling system using a heat exchanger and antifreeze being cooled by liquid nitrogen
Published: 29.01.2016
Authors: Pavlov S.K., Chugunkov V.V.
Published in issue: #1(49)/2016
DOI: 10.18698/2308-6033-2016-1-1461
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts