Vendetta Final Proposal Part 2 - Cal Poly
Vendetta Final Proposal Part 2 - Cal Poly
Vendetta Final Proposal Part 2 - Cal Poly
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11 Performance<br />
11.1 Specific Excess Power Requirements<br />
Compliance with RFP specific excess power requirements is best shown using specific excess power envelopes<br />
including those required as measures of merit. Figure 11.1 shows the 1-g military specific excess power envelope. The<br />
RFP requirement of 0 ft/s at Mach 1.6 and 50,000 ft is met with 33.7 ft/s specific excess power. The 1-g maximum<br />
(afterburner) specific excess power envelope, in Figure 11.2, shows that the RFP requirement of 200 ft/s is met with a<br />
value of 212.5 ft/s. This envelope also shows that the maximum Mach number at 36,000 ft measure of merit is 2.18.<br />
The 2-g maximum specific excess power envelope, in Figure 11.3, shows that the RFP requirement of 0 ft/s is met with a<br />
value of 8.0 ft/s. This requirement is design driver for the thrust produced by the propulsion system. The 5-g maximum<br />
specific excess power envelope and maximum sustained load factor envelope required as measures of merit are shown in<br />
Figure 11.4 and Figure 11.5 respectively.<br />
70,000<br />
60,000<br />
RFP Requirement 0<br />
50,000<br />
P s = 0 ft/s<br />
Altitude (ft)<br />
40,000<br />
30,000<br />
Stall Limit<br />
50<br />
100<br />
150<br />
150<br />
200<br />
20,000<br />
10,000<br />
Flaps<br />
200<br />
300<br />
400<br />
q Limit<br />
0<br />
0 0.5 1 1.5 2 2.5<br />
Mach<br />
Figure 11.1 - 1-g Military Specific Excess Power Envelope at Maneuver Weight<br />
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