1. An Analysis of Ramjet Engines Using Supersonic Combustion;Weber;NACA TN,1958
2. The Theoretical Computation of Equilibrium Compositions, Thermodynamic Properties and Performance Characteristics of Propellant Systems;Browne;U. S. Naval Ordnance Test Station, NavWeps Rep,1960
3. Influence of injectant properties for fluid injection thrust vector control
4. LIQUID INJECTION THRUST VECTOR CONTROL