[Sample B: Approval/Signature Sheet] - George Mason University

OPERATIONAL CAPABILITY Utility for Helicopter A (HLA)
Helicopter B (HLB)
Total Difference
Total Difference
A3.2 Receiver
A1.10 Navigation
A4.4 Multirole
A1.6 Scope
A1.9 Countermeasures
A2.10 Secure
A2.8 Interoperability
A1.2 Scope
A2.9 Capacity
A1.4 Armament payload
Other
Figure 34. Comparison between Helicopter A (HLA) and Helicopter B (HLB).
Figures 35 to 39 show the results of the remaining alternatives, with their utilities
divided by the four high level fundamental objectives. For example, FTR obtained its
highest utility under the fundamental objective Force Application and the lowest under
the fundamental objective Force Support. The width of each bar is proportional to the
weight of the respective objective.
74
0.265
0.098
0.167
Helicopter B (HLB) Helicopter A (HLA)