The specific impulse Isp is by definition related to the exhaust velocity through the acceleration at sea level g0 (9.81 m/s2). For a given amount of propellant (i.e... GATE 2016 Aerospace Engineering. Q. 1 – Q. 25 ... constant and the ratio of specific heats for both the streams are 287 J/kgK and 1.4, respectively. If the fuel-​air ... f50e787ee1 adebal
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