U.S. Army Materiel Command. Engineering Design Handbook: Elements of Aircraft and Missile Propulsion

AMC Pamphlet AMCP 706-285 — Headquarters, U.S. Army Materiel Command, 1969. 529 p.Classification of Propulsion Engines.
Rocket-propelled Weapons.
Flow Processes in Jet Propulsion Engines.
Integral Equations for Isentropic Flow Functions.
Applied to Two Arbitrary Cross-sections of.
Flow Channel.
Isentropic Functions for the Flow of Ideal Gases.
Equations for Computing Fanno Flow Functions for.
Ideal Gases.
Properties of Double-base Propellants.
Binders for Composite Propellants.
Oxidizers for Composite Propellants.
Typical Composite Propellant Formulations.
Some Effects Due to Acoustic Instability in a Solid.
Principal Conclusions from Experiments Concerned.
Methods for Suppressing Acoustic Instability (Solid Propellant Rocket Motor With Acoustic Instability Propellant Rocket Motors).
Calculated Specific Impulses for Several Liquid.
Propellant Systems.
Physical Properties of Water Solutions of Hydrogen Peroxide.
Physical Properties of Several Liquid Oxidizers.
Physical Properties of Oxides of Nitrogen.
Physical Properties of Several Oxidizers Containing.
Fluorine and Oxygen.
Physical Properties of Liquid Fuels.
Physical Properties of Light Hydrocarbon Fuels.
Performance of Hybrid Fuels With Fluorine and Oxygen.
Performance of Hybrid Fuels With Hydrogen Peroxide Oxidizers.
Chlorine Trifluoride Oxidizers.
Classification of Air-breathing Engines.
Army Aircraft and Their Engines.
Values of Loss in Specific Output (Ahrn ) As a Function of Regenerator Effectiveness (eR).
Critical Pressure Pa and Critical Temperature . for Several Gases.
Relationships Between Dependent Flow Variables and the Friction Parameter.
Changes in the Flow Variable With Increase in Flow.
Mach Number.
Equations for Conditions Along a Fanno Line.
Compressible Flow Functions for Isentropic Flow.
Compressible Flow Functions for Fanno Flow.
Compressible Flow Functions for Rayleigh Flow.
Compressible Flow Functioqs for Normal Shock Waves.
Abbreviations for Principal Units of Measurement.
Systems of Dimensions. Their Units and Conversion Factors.
Conversion Factors (American Engineers System of Units).
Dimensional Formulas and Units.
Functions of the Specific Heat Ratio y.
Values of (Pg /Pe) ''.
Values of the Parameter dt = (Pe/Pg ) Y''~.
Values of the Parameter.
Molar Specific Heats at Constant Pressure for C-H-NO Compounds.
Function of PZ /Pe.
Enthalpy of C-H-N-0 Compounds above To= 298.16"K.