This category helps you to calculate the propulsion numerical related to pressure, entropy, efficiency, etc., – WINGS OF AERO
Specific Heat for an Ideal Gas at Constant Pressure and Volume. This represents the dimensionless heat capacity at constant volume; it is generally a function of temperature due to intermolecular forces
Shaft horsepower is determined by the rpm and the torque (twisting moment) applied to the propeller shaft. Since turboprop engines are gas turbine engines, some jet thrust is produced by…
Power delivered to the piston-driven propeller engine by the crankshaft is termed as the shaft brake power P. Actual power available is always less than the shaft brake power …
the energetic ions in the beam can charge exchange with neutral gas coming from the thruster or the neutralizer, producing fast neutrals propagating in the beam direction and slow ions…
The heated hydrogen reaches exit speeds of 16 kilometres per second (9.9 mi/s). An arc jet-propelled test satellite by the name of Baden-Württemberg