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

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CARGO (CGO) Medium lift transport aircraft Capable to be configured as a tanker (maximum of 30000 lbs of available fuel to receiver aircraft) Capable to be air refueled Chaff, flares, MAWS NVG capability INS capability Encrypted data link (>15Mbps) and voice communication (2 VHF, 2 UHF and 1 HF) and fully interoperable systems Capable to operate in semi-prepared runways (SPR) Maximum range of approximately 2700 Nm Maximum payload weight of 50000 lbs Estimated unit acquisition cost – U$ 50 million HELICOPTER A (HLA) Combat helicopter intended for close support of ground troops and attack of ground armored targets Capable to be air refueled Chaff, flares, RWR NVG capability INS capability Encrypted data link (>15Mbps) and voice communication (2 VHF and 2 UHF) and fully interoperable systems Maximum combat radius of 130 Nm (A/G and A/A) 30mm cannon capable to engage targets in the ground and in the air Maximum external armament payload of 2000 lbs AWX A/G capability Estimated unit acquisition cost – U$ 6 million 126
HELICOPTER B (HLB) Light attack helicopter with SAR capability Flight characteristics suitable to be used in basic formation of helicopter pilots No data link and encrypted communication (only 2 VHF) No AWX and NVG capability Maximum combat radius of 100 Nm (A/G) Maximum external armament payload of 2000 lbs No auto-defense systems Capable to transport 2 litters in SAR configuration ANTI SUBMARINE WARFARE (ASW) Long range anti submarine warfare patrol aircraft Submarine detection sensors such as directional frequency and ranging (DIFAR) sonobuoys and magnetic anomaly detection (MAD) equipment Anti surface torpedoes, missiles and mines Chaff, flares, RWR High endurance (approximately 12 hours) INS capability Encrypted data link (>15Mbps) and voice communication (2 VHF, 2 UHF and SATCOMM) and fully interoperable systems Maximum combat radius of 1300 Nm for all misisons Maximum armament payload for anti ship mission - 6000 lbs Maximum armament payload for anti submarine mission -18000 lbs AWX A/G detection and engagement capability Range of detection sensors 100 Nm (surface and under surface) Estimated unit acquisition cost – U$ 36 million 127
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Comparing and Prioritizing Aircraft
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DISCLAIMER This work contains ficti
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TABLE OF CONTENTS Page List of Tabl
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LIST OF TABLES Table Page Table 1:
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Figure 36: Utilities for Cargo (CGO
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ABSTRACT COMPARING AND PRIORITIZING
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Figure 1. Map of South America. 5 R
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- according to recent estimates - c
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transportation to others organizati
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Jobim points out that the lack of r
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2.1 Systems Life Cycle in the BAF 2
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system. The generation of a POR con
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section (OPS) is subordinated to th
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According to Ralph Keeney, the stra
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3. THEORETICAL FOUNDATIONS AND METH
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the alternatives under analysis. 3.
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exhaustive representation of the me
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is met but does not directly measur
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Winterfeldt and Edwards argue that
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Moreover, the shape of the utility
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described by Kirkwood. 66 The aggre
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Additive independence is a stronger
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The multiplicative utility function
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4.1 Decision Support 4. MODEL CONST
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of the overarching objective of the
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Figure 9. Decision Frame with Funda
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Force Application Force Awareness A
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The following definitions were adop
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Engagement Attack precisely Attack
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different from engaging a target in
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Figure 19. Fundamental Objectives H
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capability to engage targets in the
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FORCE AWARENESS 2 DETECTION 2.1 INT
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4.3.2 Assumptions As described befo
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Using the objectives hierarchy in f
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The next step was to verify the add
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was found to be utility independent
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An exponential SUF formula was used
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4.3.4 Assessing weights Utility Fig
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A2.4 Endurance ranged from 0 to 5,
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5.1 Populating the Model 5. VALUE M
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to replace Helicopter B (HLB), whic
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OPERATIONAL CAPABILITY Utility for
Page 88 and 89: 1.000 Utility 0.000 Utility 1.000 0
Page 90 and 91: the information already provided by
Page 92 and 93: This type of analysis looks for poi
Page 94 and 95: The great variations in the utility
Page 96 and 97: Utility 0.560 0.000 0 100 Figure 42
Page 98 and 99: As before, the weights variations w
Page 100 and 101: used to check the effects of these
Page 102 and 103: The actual thresholds can be define
Page 104 and 105: 8. CONCLUSION Brazil is a huge coun
Page 106 and 107: Finally, this research intends to f
Page 108 and 109: 1.2 Maximize the survivability capa
Page 110 and 111: 4 Maximize the Force Support capabi
Page 112 and 113: A1.6 Scope See A1.2 A1.7 Scope See
Page 114 and 115: A 2.11 Capacity Amount of data that
Page 116 and 117: APPENDIX 3 UTILITY FUNCTIONS 1 Maxi
Page 118 and 119: 1 0.8 0.6 0.4 0.2 0 1 0.8 0.6 0.4 0
Page 120 and 121: 1.2 Maximize the survivability capa
Page 122 and 123: 2.1.2 In the surface. 1 0.8 0.6 0.4
Page 124 and 125: Utility Figure A3.17 - A2.7 Coverag
Page 126 and 127: 2.3.2 Using data 1 0.8 0.6 0.4 0.2
Page 128 and 129: 3.2 Maximize the airlift capability
Page 130 and 131: Utility 1 0.8 0.6 0.4 0.2 0 1 0 0 2
Page 132 and 133: 1Force Application 0.3208 2 Force A
Page 134 and 135: 2 Force Awareness 0.3448 3 Force Mo
Page 136 and 137: 3 Force Mobility 0.1724 4 Force Sup
Page 140 and 141: UNMANNED AERIAL VEHICLE (UAV) Medi
Page 142 and 143: South Atlantic scenario: National o
Page 144 and 145: 2. Force Awareness Table A7-3. Syst
Page 146 and 147: APPENDIX 8 GLOSSARY anti-submarine
Page 148 and 149: econnaissance aircraft - aircraft e
Page 150 and 151: REFERENCES Bizzi, Luiz Augusto, Jo
Page 152 and 153: ―IMINT - NIIRS National Image Int
Page 154 and 155: Winterfeldt, Detlof von, and Ralph
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[Sample B: Approval/Signature Sheet] - George Mason University

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