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Strategic Objective
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National Priority
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Why NASA?
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NASA Priority Score
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Capacity
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Safety and Reliability
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Efficiency and Performance
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Energy and the Environment
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Synergies with Security
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Support to Space
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Supporting Infrastructure
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Mission Alignment
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Lack of Alternative Sponsors
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Appropriate Level of Risk
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Why NASA Composite Score
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R&T Challenge
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Weight
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5
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3
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1
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1/4 each
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|
B1a
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Quiet propulsion systems
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9
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1
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3
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9
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3
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1
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90
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3
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9
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3
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9
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6.0
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540
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B1b
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Ultraclean gas turbine combustors to reduce gaseous and particulate emissions in all flight segments
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9
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1
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3
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9
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3
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1
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90
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3
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9
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3
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9
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6.0
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540
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B3
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Intelligent engines and mechanical power systems capable of self-diagnosis and reconfiguration between shop visits
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3
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9
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3
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3
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3
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1
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82
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3
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9
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3
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9
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6.0
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492
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B4
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Improved propulsion system fuel economy
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3
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1
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9
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9
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3
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1
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78
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3
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9
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3
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9
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6.0
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468
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B5
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Propulsion systems for short takeoff and vertical lift
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9
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1
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3
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3
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3
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1
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72
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3
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9
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3
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9
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6.0
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432
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B6a
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Variable-cycle engines to expand the operating envelope
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3
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1
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9
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3
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3
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9
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68
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3
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9
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3
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9
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6.0
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408
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B6b
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Integrated power and thermal management systems
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3
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1
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9
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3
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3
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9
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68
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3
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9
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3
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9
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6.0
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408
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B8
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Propulsion systems for supersonic flight
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3
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1
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3
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1
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9
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9
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50
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9
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9
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3
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9
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7.5
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375
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B9
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High-reliability, high-performance, and high-power-density aircraft electric power systems
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1
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3
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9
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3
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3
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3
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62
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1
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9
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3
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9
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5.5
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341
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B10
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Combined-cycle hypersonic propulsion systems with mode transition
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1
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1
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3
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1
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9
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9
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40
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9
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9
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3
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9
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7.5
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300
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B11
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Alternative fuels and additives for propulsion that could broaden fuel sources and/or lessen environmental impact
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3
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1
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3
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9
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3
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1
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60
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3
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3
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3
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9
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4.5
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270
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B12
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Hypersonic hydrocarbon-fueled scramjet
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1
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1
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3
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1
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9
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9
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40
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9
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3
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3
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9
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6.0
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240
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B13
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Improved propulsion system tolerance to weather, inlet distortion, wake ingestion, bird strike, and foreign object damage
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3
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9
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3
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1
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3
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1
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76
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3
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3
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3
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3
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3.0
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228
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B14
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Propulsion approaches employing specific planetary atmospheres in thrust-producing chemical reactions
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1
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1
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1
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1
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1
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9
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26
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3
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9
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9
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9
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7.5
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195
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B15
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Environmentally benign propulsion systems, structural components, and chemicals
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1
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1
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1
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9
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3
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1
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44
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3
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3
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3
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3
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3.0
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132
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B16
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Reduced engine manufacturing and maintenance costs
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3
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3
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3
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3
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3
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1
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52
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3
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1
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1
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3
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2.0
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104
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