Apollo 204 Review Board Appendix C Section 2 - NASA's History ...

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Z 0 L,,) uJ Z o Z I u_l ,,J :D m 4.3.3.3 I_,3.3._ 24,000 22,000 20,000 18,000 16,000 14,000 12,000 10,000 8,000 6,000 4,000 2,000 SMZA-03-SC012 APOLLO OPERATIONS HANDBOOK PERFORMANCE 0.2 0.4 0.6 • ,., I. ;1..:i RESULTSOF A SINGLE .:":ENGINE TESTAT AEDC :.3. F:T;!'
I I I I I I i I I I I I I I I ! ,[ l T 100 SMZA-03-SC01!Z APOLLO OPER.ATZONS HANDBOOK PERFORMANCE 0.8 1.0 1.2 ELAPSEDTIME IN SECONDS Figure 4-23. SPS Engine Start and Shutdown Transients 1.4 1.6 1.8 SM*2A-1099 flight by the amount of SPS fuel remaining aboard the spacecraft. (See figure14U25.) The ground controller will determine SPS engine gimbal angles if propellant leaks and/or other than nominal oxidizer to fuel ratios occur. S/C OPERATIONAL CONSTRAINTS AND LIMITATIONS. OPERATIONAL CONSTRAINTS. Attitude constraints are necessary to prevent excessive exposure of certain spacecraft surface features to solar heating, earth albedo, or deep space. These constraints are required to control temperatures for the ECS radiator inlet, S/M _CS engines, SPS propellant feedlines, and the heat shield. RCS AND SFS THRUSTING DATA-S/C OPERATIONAL CONSTRAINTS AND LIMITATIONS Basic Date. L2 Nov 1966 Revision Date Page ..... 4-_9 | |
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