MIflyer
1st Lieutenant
I do not know about pressurization. I have workd a bit on aircraft drop tank systems and the jet drop tanks are pressurized by regulating the 150 PSI bleed air down to about 12-13 PSI with a back-up feature in the regulator. We had a problem with an F-105F climbing out of Savannah that started to stream fuel very heavily and the AB caught the fuel on fire; the crew punched out and one did not survive. We found that some genius at the ALC had decided to stop changing out the auxillary fuel tank pressure regulators on a time compliance basis because "it was too much trouble." The result was there was an unknown number of regulators in the fleet that could fail at any time and in which the backup feature had sat there unmoving so long that it was frozen. Failure of the primary regulator would put 150 PSI into the tanks and that might be what occurred with that F-105F. We could not be sure that had occurred but we were sure that we had a bunch of regulators that could fail at any moment and told the F-105 units to not fly with drop tanks or the bomb bay tank operational. An F-105 without those tanks has a normal endurance of about 30 min.
In WWII the US used the exhaust of the vacuum pump that drove the flight instruments such as the artificial horizon and directional gyro. This would have been no more than 2 to 3 PSI. That is what forces the fuel out of the drop tank; there are no pumps in it. I would have thought that all the drop tanks used that same approach, so I am surprised that 200 gal tank was unpressurized.
In WWII the US used the exhaust of the vacuum pump that drove the flight instruments such as the artificial horizon and directional gyro. This would have been no more than 2 to 3 PSI. That is what forces the fuel out of the drop tank; there are no pumps in it. I would have thought that all the drop tanks used that same approach, so I am surprised that 200 gal tank was unpressurized.