A rocket nozzle is to be constructed with dimensions as


Question: A rocket nozzle is to be constructed with dimensions as shown in Fig. The following table gives the composition of the exhaust products:

448_Compound.png

The stagnation pressure is 3400 kPa and the stagnation temperature is 3000°C. The nozzle is to be constructed of graphite. The objective of the problem is to estimate the rate of erosion (ablation) of the graphite at the throat, and particularly to estimate the time elapsed for a 10 percent increase in throat diameter.

1515_11-18.png

Request for Solution File

Ask an Expert for Answer!!
Computer Engineering: A rocket nozzle is to be constructed with dimensions as
Reference No:- TGS02308060

Expected delivery within 24 Hours