Download An impartial review of the rise and progress of the by Charles Pettit PDF

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By Charles Pettit

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Read or Download An impartial review of the rise and progress of the controversy between the parties known by the names of the Federalists, & Republicans. : Containing an investigation of the radical cause of division ; and of some of the subordinate or auxiliary causes w PDF

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Extra info for An impartial review of the rise and progress of the controversy between the parties known by the names of the Federalists, & Republicans. : Containing an investigation of the radical cause of division ; and of some of the subordinate or auxiliary causes w

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Chamber pressure decay 5. Low chamber pressure. After investigating the anomalies and performing a series of tests to verify the assumed causes of the problems, it was concluded that the high propellant temperature and low chamber p r e s s u r e anomalies warranted remedial action to preclude possible future mission problems. The testing at MSFC verified that the 501 flight APS gradual chamber pressure decay and oscillations, noted in the latter portion of the mission, were a direct result of the high propellant temperature.

_ Engine I Time - ~~ 0-10 900 sec* Engine 2 - Engine 3 ~. 2 pulses/ 100 sec 8 pulses/ 100 sec Ipulse/ 250 sec 14 pulses/ 100 sec 8 pulses/ 100 sec 25 pulses/ 100 sec Ipulse/ 1 pulse/ 95 sec I pulse/ 66 sec 660-750 see 10 900-12 660 sec" I 1 160-11 490 sec 12 660-19 800 sec" I 1 0 sec ~~ '$ Pulse Width 26 = 65 milliseconds . ~ Engine 4 g 100 v) v) W pc n 160 h LL 0 v w pc 120 TEMPERATURE 3 c 4 n! W n 3 80 c 40 100 ELAPSED TEST TIME (SEC) FIGURE I O . _- -- ELAPSED T€ST TIME (SEC) FIGURE 11. ENGINE 2 Pc, INJECTOR TEMPERATURE, AND OXIDIZER SUPPLY TEMPERATURE VERSUS TEST TIME I 120 A 1 E Y w iw loo 240 Y, G!

065 4. 0 33 2. 065 25 6. the Pc decay appeared to be m o r e dependent on engine hardware temperature than on oxidizer temperature, since the Pc decay occurred during the latter portion of the duty cycle at which time the engine temperatures w e r e at peak values. (Note: Pc decreases of 7 to 12 psia w e r e noted in the subject tests. 1 Although the data did not yield a good indication of the direct effect of oxidizer inlet temperature, it did show that this temperature significantly influenced the engine hardware temperature.

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