Which one of the following is a hypergolic propellant combination used in rocket engines?
(A) Liquid hydrogen - liquid oxygen
(B) Unsymmetrical dimethyl hydrazine - nitrogen tetroxide
(C) Rocket fuel RP-1 - liquid oxygen
(D) Liquid hydrogen - liquid fluorine
Which one of the following is a hypergolic propellant combination used in rocket engines?
(A) Liquid hydrogen - liquid oxygen
(B) Unsymmetrical dimethyl hydrazine - nitrogen tetroxide
(C) Rocket fuel RP-1 - liquid oxygen
(D) Liquid hydrogen - liquid fluorine
In aircraft engine thermodynamic cycle analysis, perfectly expanded flow in the nozzle means that the static pressure in the flow at the nozzle exit is equal to
(A) the stagnation pressure at the engine inlet.
(B) the stagnation pressure at the nozzle exit.
(C) the ambient pressure at the nozzle exit.
(D) the static pressure at the nozzle inlet.
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