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Preliminary MHD Business Plan
Gary V Stephenson
Seculine Consulting
20 August 2008 – Outline Only Version
Engineering
Physics
Alternatives
Disclaimer: This briefing contains forward looking statements & does not constitute investment advice.
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Executive Summary
• A four phase enhancement plan is proposed, to incorporate magneto-hydrodynamic (MHD) devices into our air travel manufacturing infrastructure and products in these stages:
1. MHD Control Surface Development, 2009 – 2018
2. Subsonic MHD Engine Development, 2012 – 2021
3. Supersonic MHD Bypass Vehicle Development, 2018 – 2027
4. MHD designed into BWB Vehicle Development, 2018 - 2027
• The following business cases for each phase are expanded upon in this presentation:
1. MHD Control Surface Development, 2009 – 2018
2. Subsonic MHD Engine Development, 2012 – 2021
3. Supersonic MHD Bypass Vehicle Development, 2018 – 2027
4. MHD designed into BWB Vehicle Development, 2018 - 2027
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Outline
• What is MHD?
– Basic MHD Devices
– MHD as Applied to Air Flow Control
• MHD Control Surface (CS) Replacement Examples
– MHD-CS Business Plans
– MHD-CS Program: Schedule, Costs, & Returns
• MHD-Engine Concept
– MHD-Engine Business Plan
– MHD-Engine Program: Schedule, Costs, & Returns
• MHD-Bypass Concept (AJAX)
– MHD-Bypass Business Plan
– MHD-Bypass Program: Schedule, Costs, & Returns
• MHD BWB Concept (Aerodyne)
– MHD BWB Business Plan
– MHD BWB Program: Schedule, Costs, & Return
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What is MHD?
• Basic description of using electro-magnetism to control air flow goes here:
– Using Faraday force
– Using Lorentz (Laplace) force
• Include figures of both types
• Show combination, the parietal accelerator, in figure form
(use Petit’s “Silence Barrier” pp 35-36 as reference)
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Basic MHD Devices
MHD Devices create effects identical to mechanical disturbances:
– MHD accelerators for creating a divergent region via expansion
– MHD decelerators to creating a convergent region via compression
• Include small figures of both
(use Petit’s “Silence Barrier” pp 39-40 as reference)
• First Order Applications:
– Turbulence reduction in all regimes
– Drag reduction in all regimes
– Friction heating reduction in all regimes
– Sonic boom mitigation in supersonic regimes
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MHD Control Surface (CS) Application
• Replacement of Mechanical AileronsAilerons using MHD accelerators and decelerators
– Include figure to show configuration
• Replacement of Mechanical RudderRudder using MHD accelerators and decelerators
– Include figure to show configuration
• Replacement of Mechanical FlapsFlaps using MHD accelerators and decelerators
– Include figure to show configuration
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MHD-CS Business Plan
• Product: Electromagnetic replacements for all commercial control surfaces
• Development timeline: 2009 – 2018
• Technical advantages: dramatically reduced drag for better fuel efficiency
• Cost advantages: fuel savings via drag reduction
• Technical challenges: weight and power needs may cancel much of the fuel savings
• Post development market: widespread commercial deployment
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MHD-CS Program:
Schedule, Costs, Returns
• Major milestones:
Include cost/return chart here
2008 2010 20142012
IRAD Funding
GO-NOGO
0.1 MHD Survey / Teaming
0.2 Fund External Academic Research
0.3 Fund Internal Research and Devl
2016 2018 2020
Devl
GO-NOGO
1.1 MHD Lab Devl
1.2 MHD Device Risk Reduction Issues Lab
Ready1.3 MHD CS Device Devl & Test
• Projected costs and returns:
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Air-breathing MHD Engine Concept
• Include conceptual drawing of Lorentz force MHD engine
• Include descriptions and figures describing both retrofit (in cowling) MHD engines & integrated MHD engines
• Application: Commercial Aircraft Engine Replacements
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MHD Engine Business Plan
• Product: Electrically powered retrofit air breathing subsonic engines on all commercial aircraft
• Development timeline: 2012 – 2021
• Technical advantages: Powered by hydrogen fuel cells or other electrical source; no need of hydrocarbon fuels
• Cost advantages: Electrical power less expensive than hydrocarbon based fuels in long run
• Technical challenges: No record of subsonic operation for airbreathingengines – normally need very low pressures (some published testing with watercraft, & Biefeld-Brown electrostatic ionizing motors)
• Post development market: widespread commercial deployment
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MHD Engine Program:
Schedule, Costs, & Returns
• Major milestones:
Include cost/return chart here
2016 2018 2020 2022 2024 2026 2028 2030
Engine Lab
PDR CDR
MHD Engine Test & ProduceMHD Engine Risk Reduction
Flight Test
GO-NOGO
2.1 MHD Lab Devl & Conceptual Design
Flight Test
GO-NOGO
• Projected costs and returns:
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MHD Bypass Concept
• History: Russian AJAX Concept
• Application: SSTO
• Include description and illustration
• Include STAIF references
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MHD Bypass Business Plan
• Product: Matched MHD generator on intake and MHD accelerator on exhaust of a conventional SCRAM jet to enable single stage toorbit (SSTO) operations
• Development timeline: 2018 – 2027
• Technical advantages: Eliminates need for second boost stage
• Cost advantages: Inexpensive entry to LEO via fully reusable vehicle
• Technical challenges: Very high powers in bypass; very high Mach number operation for SCRAM jet, even with bypass
• Post development market: LEO launch, or GEO launch with IUS
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MHD Bypass Program:
Schedule, Costs, & Returns
• Major milestones:
Include cost/return chart here
• Projected costs and returns:
Conceptual Design Devl & Flt Test
PDR
2022 2024 2026 2028 2030
Cert for
flight
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MHD BWB Concept
• The “Aerodyne”
• Include description and illustration
• Application: Long Term Commercial Flight Replacement
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MHD BWB Business Plan
• Product: A blended wing body (BWB) airframe with the MHD propulsion completely integrated with the skin of the aircraft
• Development timeline: 2018 – 2027
• Technical advantages: extremely low drag, with low noise signature for less impact on urban environments
• Cost advantages: very low drag dramatically improves efficiencies
• Technical challenges: would not be airworthy under a loss of power; would need safety parachute
• Post development market: unlimited, but long term (20+ years before development is complete)
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MHD BWB Program:
Schedule, Cost, & Return
• Major milestones:
Include cost/return chart here
• Projected costs and returns:
Conceptual Design Devl & Flt Test
PDR
2022 2024 2026 2028 2030
Cert for
flight
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MHD Multi-Program
Integrated Schedule
• Integrated schedule uniformly spreads MHD workload to facilitate smooth, slow growth personnel and facilities.
2008 2010 2012 2014 2016 2018 2020 2022 2024 2026 2028 2030
MHD IRAD
Development Phases
MHD Control Surface Devl
MHD Engine Devl
MHD BWB AerodyneMHD Engine
GO-NOGO
MHD BWB
GO-NOGO Flight
Test
GO-NOGOMHD Devl
GO-NOGO
Cert for
Flight
MHD BWB
GO-NOGO
• Major milestones:
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Conclusions / Suggested Way Forward
• Preliminary business plans show the viability of developing:
– MHD control surfaces,
– subsonic MHD engines,
– supersonic MHD bypass engines,
– and an MHD BWB concept.
• Suggested way forward:
– Partner with MHD researchers in academia to begin detailing device related physics, fabrication, and device wind tunnel testing
– Develop an IRAD program focusing on MHD technologies
– Conduct a make / buy trade on MHD devices to determine what to outsource
– Develop a supplier base that is willing to supply MHD devices for early control surfaces
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Backup Slides
Gary V Stephenson
Seculine Consulting
20 August 2008 – Outline Only Version
Engineering
Physics
Alternatives
Disclaimer: This briefing contains forward looking statements & does not constitute investment advice.
_____S_E_C_U_L_I_N_E_______C_O_N_S_U_L_T_I_N_G_____P_R_O_P_R_I_E_T_A_R_Y_____
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2008 2010 2012 2014 2016 2018 2020 2022 2024 2026 2028 2030
MHD IRAD
MHD Development - Integrated Design Schedulegvs-20Aug08
Engine Lab
PDR
Development Phases
MHD IRAD Tasks
MHD Control Surface Devl
MHD Engine Devl
MHD BWB AerodyneMHD Engine
GO-NOGO
MHD BWB
GO-NOGO Flight
Test
GO-NOGOMHD Devl
GO-NOGO
IRAD Funding
GO-NOGO
CDR
MHD Engine Test & ProduceMHD Engine Risk Reduction
Flight Test
GO-NOGO
Cert for
Flight
Devl
GO-NOGO
MHD Control Surface Development Tasks
MHD Engine Development Tasks
MHD BWB / Aerodyne Development Tasks
MHD BWB Aerodyne Conceptual DesignDevl & Flt Test
PDR Cert for
flight
0.1 MHD Survey / Teaming
0.2 Fund External Academic Research
0.3 Fund Internal Research and Devl
1.1 MHD Lab Devl
1.2 MHD Device Risk Reduction Issues Lab
Ready1.3 MHD CS Device Devl & Test
2.1 MHD Lab Devl & Conceptual Design
MHD BWB
GO-NOGO
Flight Test
GO-NOGO