Non per fare dietrologia, ma questo post, dopo la sua pubblicazione ha avuto una sorte stranissima. Ho dovuto riscriverlo e ripubblicarlo da capo, dopo avere cambiato password al mio accesso a Google. Il "problema" molto molto divertente che si era verificato al suo codice Html dà molto di che pensare: in cinque anni di blogging non avevo mai visto niente del genere!
Alea iacta est, Iaea augenda est.
Ringrazio Francesco Celani ed Emanuele F. Marano per avermi guidato oggi -- come Virgilio il Poeta -- al "Paradiso" di chi da anni sa che la fusione fredda e le LENR sono realtà. Il “Paradiso” di chi ha subìto il dileggio delle menti tetragone che rifiutano di guardar nel cannocchiale o in mala fede⎯ fanno porcherie d'ogni genere pur di celarne l'esistenza.
È un paradiso incommensurabile. Include le frontiere della scienza esotica, dove persino le LENR sono solo uno di tanti paragrafi. Un paragrafo che si apre così:
3.1.5 Low Energy Nuclear Reactions
3.1.5.1- Electrochemically Induced Deuterium Fusion in Palladium The first-discovered form of solid-state fusion was that achieved by electrochemically splitting heavy water in order to cause the deuterium to absorb into pieces of palladium metal. When this experiment is conducted according to procedures that have resulted from the work of many researchers since 1989, it is reproducible.
The evidence that a nuclear process is occurring is that excess energy inthe form of heat (greater than what could be produced by any possible chemical reaction in the system) and helium 4 (He4) (in quantities exceeding any possible contamination) occur. The primary nuclear reaction is:
1D2 + 1D2 = 2He4 + heat
E si conclude una decina di pagine dopo così:
3.1.7 Radiution Hazard Considerations
As explained in Section 3.1.4.8, radiation hazards associated with any conventional nuclear reaction-based vehicle propulsion system are highly significant. By contrast, most of the nuclear reactions discussed in this report are of a fundamentally different type, which produce radiation levels that are orders of magnitude less (for an equivalent release of energy) as compared to traditional types of nuclear reactions.
Deuterium-based solid-state nuclear reactions emit low levels of neutrons and gamma rays; however, an aqueous-based system is unlikely to be developed into part of an aircraft P/P system because the operating temperature is not high enough.
Based on claims from the U of I research team, if PPCs (Section 3.1.5.3) could be developed into a power source for an aircraft P/P system, they would provide absolutely no hazard to operations/maintenance personnel or passenger because:
- the initial fuel and matrix materials are not radioactive;
- no neutrons or gamma rays are produced by the hypothesized fusiordfission reaction; and
- alpha particles (He4 nuclei), Beta particles (electrons), and recoil fission products (newly created elements) are of low enough energies to be easily shielded.
In the event of a catastrophic event (crash) severe enough to shatter the PPC containers, residual radiation emitted by the nickel/tanium matrix (and resulting new reaction product elements, which had been created until that time) would be so low that it would not be a problem. The U of I team claims that the residual (Beta) radiation is at such an extremely low intensity that substrates from PPCs (that had been operating until the time of measurement) must be wrapped in ultrahigh-speed photographic film for several weeks in order to cause noticeable fogging of that film.
The alternative tradeoff for a crash scenario for an aircraft propelled by these new types of nuclear reactions should be noted. In contrast to a chemical fuel powered aircraft, there would be no spilled LH2 or hydrocarbon fuel and the resulting fire.
La sezione successiva invece comincia così:
3.2 Energy Conversion
Some of the energy produced by any energy producing system will be in the form of heat. This section presents the results of current research into advanced methods of converting a higher fraction of heat to electric power than may be accomplished with current technology. The electric power may then be used in an aircraft P/P system to provide propulsion.
Additionally, a newly discovered method of transferring relatively large amounts of heat (without a temperature gradient) is described. This technology allows heat exchanger weights and volumes to be reduced and reliability to be significantly increased and is suitable for a very wide range of technical applications.
Insomma, cari ingegneri, fisici e appassionati di scienza che seguite 22 passi d'amore: avete circa 200 pagine da leggere per tutto il restodell'estate e approfondire ben oltre! Fatelo iniziando a scaricare questi due libri (pdf):
- Advanced Energetics for Aeronautical Applications (20 Mb)
- Advanced Energetics for Aeronautical Applications; Volume II (2 Mb)
E occhio a non fare fuori tutta la banda del NASA Technical ReportsServer (NTRS)!
Magari provate a scaricarli anche dal mio Google Docs, così non si creano problemi:
Mentre il download procede, leccatevi i baffi con gli indici; quello del secondo libro vi sorprenderà forse ancora più di quello del primo. E se tutto questo è materiale pubblico, figuriamoci cosa diavolo può essere secretato.
Benvenuti a un Sacro Graal che ci introduce alla Nuova Fisica, quella che gli scienziati mainstream ci hanno sempre detto "non esiste". Non si scappa: o sono ignorantoni senza speranza o sono bugiardi matricolati! Comunque sia vanno scacciati dai templi del Sapere.
NASA / CR-2003-212169
Advanced Energetics for Aeronautical Applications
1. Potential New Aeronautical Energetic Requirement. The "Emissionless Aircraft"
1 .1 Current State-of-the-Art Transport Aircraft
...1.2 Water Vapor/Cloud Formation Problem (with other pollutants)
...1.3 Emissionless Approaches
.........1.3.1 Energy Storage
.........1.3.2 Beamed Energy
.........1.3.3 Chemical Propulsion
...1.4 Energy Conversion Approaches
.........1.4.1 Heat Engine
.........1.4.2 Thermophotovoltaic Technology
.........1.4.3 Electrochemical Processes
2. The Fuel Cell Energy Conversion Approach
...2.1 Fuel Cells
.........2.1.1 Types of Fuel Cells (Lithium vs. Hydrogen)
.........2.1.2 Types of Hydrogen Fuel Cells
.........2.1.3 Hydrogen Fuel Cells for Vehicular Applications
...2.2 Hydrogen Storage
.........2.2.1 Elimination of All Methods Except Liquid Hydrogen
.........2.2.2 Liquid Hydrogen Supplied in Preloaded Tanks
...2.3 Electric Motors
.........2.3.1 Design for a 40-MW Motor
.........2.3.2 Motor Controller Strategy
.........2.3.3 Inapplicability of Superconducting Technology
...2.4 Advanced Aerodynamics
.........2.4.1 Strut-Braced Wings
.........2.4.2 Riblets for Fuselage Drag Reduction and Increased Heat Transfer
.........2.4.3 Fuselage Skin Heating
.........2.4.4 Winglets
.........2.4.5 Laminar Flow Control
...2.5 Structural Weight Reduction
.........2.5.1 Carbon Nanotubes
.........2.5.2 Other Reduced Weight Materials
...2.6 The NASA-LaRC Flight Optimization System Code
.........2.6.1 Input and Output Parameters
...2.7 System Results
.........2.7.1 Emissionless Aircraft P P Systems Based on Planar Solid Oxide Fuel Cells
.........2.7.2 Component Weight Summary
.........2.7.3 Typical FLOPS Code Calculations for the Emissionless Aircraft Concept
.........2.7.4 PowerPropulsion System Component Placement
.........2.7.5 Particular Features of this Conceptual Design
.........2.7.6 Tradeoff Fraction of Retained Water vs. Aircraft Weight
.........2.7.7 Discussion of Selected Emissionless Aircraft Components
.........2.7.8 FLOPS Calculation Maximum Range Results
.........2.7.9 FLOPS Calculation Maximum Range Results-if Liquid Water is Expelled-The "Weinstein Approach"
...2.8 Other Organizations Developing Fuel Cells for Aviation Applications
.........2.8.1 FASTec Electric Plane
.........2.8.2 Boeing Fuel Cell Auxiliary Power Unit
3. Midterm Energetics and Advanced Technology Alternative Approaches
...3.1 Advanced Energetics
.........3.1.1 High Energy Density Material Fuels
.........3.1.2 High Energy Hydrogen Atom Systems
.........3.1.3 Nuclear Isomers for Energy Storage
.........3.1.4 Inertial Electrostatic Confinement Fusion as a Potential Power Propulsion Source
.........3.1.5 Low Energy Nuclear Reactions
.........3.1.6 Nanofusion
.........3.1.7 Radiation Hazard Considerations
...3.2 Energy Conversion
.........3.2.1 The Thermal Diode
.........3.2.2 Supertube Enhancement of Heat Exchanger Technology
.........3.2.3 Potential Heat Exchanger Weight Reduction using Supertubes
.........3.2.4 Reliability: Supertube Heat Exchanger vs . State of the Art
...3.3 Energy Storage
.........3.3.1 Flywheels
.........3.3.2 Supercapacitors
.........3.3.3 Superconducting Magnetic Energy Storage
.........3.3.4 Possible Enhanced Superconducting Magnetic Energy Storage
4. Longer Term Advanced Concepts
...4.1 Breakthrough Propulsion Technologies
.........4.1.1 The Thornson Propulsion Device
.........4.1.2 High-Voltage Propulsion in Air
.........4.1.3 High-Voltage Propulsion in Vacuum
...4.2 Breakthrough Energy Technologies
.........4.2.1 Ultraconductors
.........4.2.2 Zero-Point Energy Concepts
.........4.2.3 Motionless Electromagnetic Generator
.........4.2.4 Longitudinal Electric Waves
...4.3 Breakthrough Physics
.........4.3.1 Background
.........4.3.2 Gravity and Gravitational Waves
.........4.3.3 Aharonov-Bohm Effect
.........4.3.4 Theoretical Electrodynamics
5. Conclusions
References
NASA/CR-2005-213749
Advanced Energetics for Aeronautical Applications: Volume II
1. POTENTIAL NEW AERONAUTICAL ENERGETIC REQUIREMENT ⎯ THE "EMISSIONLESS AIRCRAFT" ⎯ UPDATED INVESTIGATIONS AND INNOVATIONS
...1.1 Emissionless Aircraft Conceptual Model at the Conclusion of Work Prior to This Report
.........1.1.1 Status of Project Investigations when Prior Work was Published
.........1.1.2 Conceptual Design and Component Placement
.........1.1.3 Calculated Maximum Emissionless Aircraft Ranges
...1.2 Potential Planar Solid Oxide Fuel Cell Weight Reduction
.........1.2.1 Introduction
.........1.2.2 Background Information
.........1.2.3 PSOFC Parameters
.........1.2.4 PSOFCs Based upon Superalloys
.........1.2.5 Plate Bending and Plasticity Analyses
.........1.2.6 Calculation Method for Plate Bending and Plasticity Analyses
.........1.2.7 Calculation Assumptions
.........1.2.8 Calculation Results
.........1.2.9 Preliminary PSOFC Plate Bending Analysis Conclusions
.........1.2.10 Potential PSOFC Metals
...1.3 State-of-the-Art Vendor-Supplied Planar Solid Oxide Fuel Cell Parameters
.........1.3.1 Introduction
.........1.3.2 Updated PSOFC Parameters
.........1.3.3 Discussion of Updated PSOFC Parameters
.........1.3.4 Updated Flight Optimization System Code Calculations
.........1.3.5 Procedure Used for FLOPS Code Calculations
.........1.3.6 FLOPS Code Results with Updated PSOFC Parameters
.........1.3.7 Discussion of Updated Calculated FLOPS Results
...1.4 Controlled Water Expulsion
.........1.4.1 Introduction—Water Expulsion—Major Parameters Needing Investigation
.........1.4.2 The Advantages of Water Expulsion as Vapor
...1.5 Thrust Produced by Power Recovery Turbine Exhaust
.........1.5.1 Introduction
.........1.5.2 Thrust Calculation
...1.6 Flight Optimization System Code Calculations for Various Water Expulsion Scenarios
.........1.7 Circulation Control
.........1.7.1 Introduction
.........1.7.2 Relevant Information
2. BREAKTHROUGH FUSION REACTORS AS POWER SOURCES FOR AIRCRAFT
PROPULSION
...2.1 Introduction and Background
...2.2 The Colliding Beam Fusion Reactor
.........2.2.1 Introduction
.........2.2.2 Approach for Modifying the Original CBFR Concept for the Emissionless Aircraft Application
.........2.2.3 Relevant Power and Weight Parameters of the Space Propulsion CBFR as Modified for the Proposed Emissionless Aircraft Application
.........2.2.4 Component Masses and Power Levels for the Fusion-Powered Aircraft Performance Calculations
...2.3 Heat Transfer from the Colliding Beam Fusion Reactor Surface
.........2.3.1 Introduction
.........2.3.2 Parameters for the Heat Transfer Calculation
.........2.3.3 Calculation Approach
.........2.3.4 Calculation Method
.........2.3.5 Heat Transfer Equations
.........2.3.6 Calculation Results
.........2.3.7 Heat Conversion to Additional Electric Power
...2.4 Hybrid Colliding Beam Fusion Reactor Aircraft Propulsion—The "Turbojet" Concept
.........2.4.1 Introduction2.4.2 Input Parameters for Turbojet Calculations
.........2.4.3 General Assumptions for Turbojet Calculations
.........2.4.4 Turbojet Calculation Approach
.........2.4.5 Specific Turbojet Calculation Assumptions
.........2.4.6 Calculations
.........2.4.7 Turbojet Thrust Fraction
.........2.4.8 Estimated Total Engine Weight
.........2.4.9 Effect of Turbojet Thrust on Aircraft Performance Parameters
.........2.4.10 Comments on Power Levels
.........2.5 Calculated Aircraft Range per Pound of Fuel
...2.6 Heat Transfer from the Inner Fusor Grid
.........2.6.1 Introduction
.........2.6.2 Calculation of Rate of Heat Produced in the Inner Wire Grid
.........2.6.3 Calculation of the Liquid Flow Rate Required to Control the Temperature of an Inner Grid Constructed of Tubing
.........2.6.4 Required Flow Rate and Pressure Parameters to Cool a High-Power Fusor Inner Grid
.........2.6.5 Heat Exchanger Weight to Remove Fusor Inner Grid Heat from the Aircraft
.........2.6.6 P/P System Weight and Effect on Aircraft Power Levels, Energy per Nautical Mile, and Cruise Range
3. ADVANCED ELECTRIC CONCEPTS
...3.1 Introduction and Overview
.........3.1.1 Dr. Charles P. Steinmetz's Theories of Electricity
.........3.1.2 Longitudinal and Transverse Electric Waves
.........3.1.3 Scalar Waves
...3.2 Teachings on Electric Phenomena by Dr. Charles P. Steinmetz
.........3.2.1 Introduction
.........3.2.2 Dr. Steinmetz's Teaching on Electric Transients
.........3.2.3 Dr. Steinmetz's Teaching on the Electric Field
...3.3 Differences Between Longitudinal and Transverse Electric Waves
.........3.3.1 Introduction
.........3.3.2 Definitions
.........3.3.3 Wave Propagation Velocity Differences
.........3.3.4 Transverse Waves vs. Longitudinal Waves: Transmission Line Characteristics
.........3.3.5 Unique Characteristics of Longitudinal Electricity
.........3.3.6 Demonstration of Tesla's Radiant Energy Patents
.........3.3.7 Long-Range Longitudinal Wave Transmission
...3.4 Scalar Waves
.........3.4.1 Introduction
.........3.4.2 Dr. Thomas Valone's Writings on Scalar Waves
.........3.4.3 Dr. Konstantin Meyl's Teachings on Scalar Waves
.........3.4.4 The Polarization Synchrotron
4. BREAKTHROUGH ENERGETICS — ZERO POINT ENERGY
...4.1 Introduction and Overview
...4.2 Accessing or "Tapping" Energy from Zero Point Energy
.........4.2.1 Specific Disclaimer Regarding ZPE Plausibility
.........4.2.2 ZPE Credibility Breakthrough
.........4.2.3 ZPE Access Principles Stated by Moray King
.........4.2.4 Dr. Thomas Valone's Overview of ZPE Approaches
...4.3 Zero Point Energy Principles in the Similar Technologies of Nikola Tesla and E.V. Gray
.........4.3.1 Dr. Peter Lindemann
.........4.3.2 ZPE Principles Suggested in E.V. Gray's Technology
.........4.3.3 The Energy Science of Dr. Nikola Tesla
.........4.3.4 Dr. Lindemann's Definition of "The Electro-Radiant Event
.........4.3.5 Comparing E.V. Gray's Technology with that of Tesla
.........4.3.6 Summary of Principles for Accessing ZPE
...4.4 Additional Inventions and Discoveries Claiming "Excess" Energy
.........4.4.1 Introduction
.........4.4.2 Disclaimer
.........4.4.3 The Papp Engine
.........4.4.4 The Graneaus' Water Arc Explosion Experiments
.........4.4.5 Dr. T. Henry Moray's Energy Device
.........4.4.6 Summary
5. OTHER RESEARCH RELEVANT TO ADVANCED ENERGETICS
...5.1 Introduction
...5.2 The Fourth Law of Motion
.........5.2.1 Introduction
.........5.2.2 Specific Disclaimer for the Fourth Law of Motion
.........5.2.3 The Origin of the Fourth Law
.........5.2.4 Nonsimultaneity
.........5.2.5 Third Derivative Equations of Motion
.........5.2.6 Third Derivative Reactionless Propulsion System
.........5.2.7 Overview of Patented Reactionless Propulsion Devices
.........5.2.7 Overview of Patented Reactionless Propulsion Devices
.........5.2.8 Analogy with Work Produced by Electrical Alternating Current
.........5.2.9 Statement of the Fourth Law of Motion
...5.3 The Scientific Theories of Edwin Yates Webb, Jr
.........5.3.1 Introduction
.........5.3.2 Specific Disclaimer for Webb’s Theories
.........5.3.3 Webb’s Electric Field Interpretation of Matter and Energy
.........5.3.4 Webb’s Analysis of the Null Results of Classical Aether Detection Experiments
.........5.3.5 Consequences of Removing the Aether from 20th Century Theoretical Physics
.........5.3.6 Webb’s Theory of Gravity
.........5.3.7 Comments on Webb’s Theory of Gravity
...5.4 Condensed Matter Nuclear Science
.........5.4.1 General Background and Introduction
.........5.4.2 Disclaimer for Condensed Matter Nuclear Science
.........5.4.3 Electrochemically Induced Deuterium Fusion in Palladium
.........5.4.4 The ICCF-10 Paper by Drs. Dennis G. Letts and Dennis J. Cravens, "Laser Stimulation of Deuterated Palladium: Past and Present"
.........5.4.5 The ICCF-10 Paper by Dr. Yasuhiro Iwamura, et al., "Low Energy Nuclear Transmutation in Condensed Matter Induced by D2 Gas Permeation through Pd Complexes: Correlation Between Deuterium Flux and Nuclear Products"
.........5.4.6 The ICCF-10 Paper by H. Yamada, et al., "Analysis by Time-of-Flight Secondary Ion Mass Spectroscopy for Nuclear Products in Hydrogen Penetration through Palladium"
...5.5 High Frequency Gravitational Waves
.........5.5.1 Introduction
.........5.5.2 Disclaimer for HFGWs
.........5.5.3 Extreme Weakness of Gravity and GWs
.........5.5.4 GWs
.........5.5.5 HFGWs
.........5.5.6 Applications of HFGWs
.........5.5.7 Selected HFGW Conference Papers
6. CONCLUSIONS
7. REFERENCES
E se siete ancora scettici:
E se siete ancora scettici:
There is a rumor that Defkalion is not working with you anymore. Is it true?
Best,