Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant.

Author:	Gordon, Sanford.
Additional Authors:	Huff, Vearl N.
Year:	1956
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/E56A13a
Series:	NACA research memorandum ;
Report Number:	RM E56A13a
Subjects:	Oxygen
	Fluorine
	Rockets (Aeronautics)--Fuel--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086463877