Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine /, by Edward W. Otto et al.

Title:	Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine /
Author:	Otto, Edward W.
Author:	Flage, Richard A.
Author:	Lewis Research Center
Note:	Washington, [D.C.] : National Aeronautics and Space Administration, 1959

Link:	page images at HathiTrust
No stable link:	This is an uncurated book entry from our extended bookshelves, readable online now but without a stable link here. You should not bookmark this page, but you can request that we add this book to our curated collection, which has stable links.

Subject:	Specific impulse
Subject:	Mass flow rate
Subject:	Turbine pumps
Subject:	Rocket engine design
Subject:	Propulsive efficiency
Subject:	Propulsion system performance
Subject:	Propellant tests
Subject:	Monopropellants
Subject:	Rocket engines
Subject:	Liquid propellant
Subject:	Engines
Subject:	Oxygen
Subject:	Hydrogen
Subject:	Hydrazines
Subject:	High energy propellants
Other copies:	Look for editions of this book at your library, or elsewhere.