Shall we dance under tonights stars or those of the past or the future? Let's speak of the 'physical' travel in time. Let's build the 'machine'.
Time/Space Aperture Design
<Large Scale>
NOTE: Small scale systems can be built that emulate the following assemblage of full scale systems. Notable differences is a) energy sources, b) alignment within (or doing away with) the PAAP, c) building a vacuum 'shell' to house the TSA, d) magentic field generation.
Large Scale Aperture systems are located in space outside the orbit of the Moon for several reasons.
1 Allows for a more ‘clean' environment and minimal contamination affects
2 Allows for use/manipulation of high momentum target device system and therefore application of the TSA as a true time-space transport augmentation system
3 Minimizes need for high vacuum environments, difficult to establish and control in a atmospheric environment
4 Minimizes amount of materials needed to assure system rigidity and strength
5 Minimizes potential negative affects based on radiation, time rift, gravimetric and unknown risks
6 Enhances functionality of the Primary Aperture Alignment Platform and minimizes any associated equipment needed for target alignment and insertion into the Time Space Aperture.
The Time Space Aperture (TSA) is designed based upon a combination of known and theoretical sciences to develop a method to ‘transport' an object through time. As identified in the study of black-hole singularities, an extreme gravitational field is generated with a known event horizon within the aperture. The gravimetric field is allowed to rotate along the primary axis within the aperture in a method to move the target device either forward or backward on the time continuum. Another important feature of the TSA is allowing devices with preexisting momentum to be manipulated. This adds the functionality of ‘space' into the aperture's functionality. This, thereby, gives the TSA the ability to either time displace a target and/or give the target
Definitions
High Density Laser Alignment System (HDLA) - Laser array used in conjunction with the VLAPFM for device alignment within the PAAP and as part of the optical data link telemetry system.
Primary Aperture Alignment Platform (PAAP) - Entry device for the Time Space Aperture
Time-Space Aperture (TSA) - device used to modify time continuum and inject device through the time/space event horizon
Time-Space Torroidal Focal Field (TTFF) - Time-space modified envelope which allows time travel
Synchronous Event Field Generator (SEFG) - Circumferential mounted Tokomak fusion reactors around the TSA which have a ‘open' core design. The ‘open' core design allows for the development of high magnetic field density development as well as modifying flux direction and field confinement. It also allows for field/flux rapid intensification using magnetic enhancement core enhancement techniques associated with solenoid theory and momentum effects.
Very Large Array Primary Focus Mirrors (VLAPFM) - Mirror system used to disperse the HDLA output for augmenting device alignment within the PAAP and as part of the TSNA.
Time Space Navigational Aid - A navigational system using doppler ranging and alignment capability of the HDLA and multi waveguide radar acquisition systems for high speed approach devices. Directs and aligns momentum devices through the PAAP and into the TSA.
Magnetic Enhancement Plasma Deposition (MEPD) - System used to deposit a micro-thin layer of magnetic property materials to the outer surface of the target device. This plasma deposition is very uniform in property and application in a vacuum/microgravity environment. It is used to increase time-space focal field effect.
Primary Aperture Alignment Platform (PAAP)
Function
The PAAP functions to assure the device entering the Time-Space Aperture (TSA) has correct and precise 3-axis alignment prior to Aperture engagement. It not only allows for physical manipulation of the devices but also allows for navigational symmetry with the TSA for devices with internal alignment capability, augmentation of autonomous alignment process and, is in essence, a ‘waveguide' for TSA entry.
Design Overview
The PAAP consists of a hexagonal cross sectional shape allowing for the greatest utilization of interior space, strength, minimal material and mass and ease in application of the HDLA/VLAPFM array and the TSNA. A 3-axis array of 8 GJ continuous/pulse lasers assisted by a VLAPFM group located on six parallel hexagonal axis and one central axis to stabilize, align and manipulate the incoming target devices. The laser alignment system (HDLA) focuses energy along the device on specified areas to cause localized, high density photon pressure. Associated with the laser alignment system, a navigational system (Time Space Navigational Aid - TSNA) , using the doppler ranging and alignment capability of the HDLA and multi- waveguide radar acquisition systems for high speed approach devices, and directs and aligns momentum devices through the PAAP and into the TSA. If necessary (based upon the target device's configuration), the Magnetic Enhancement Plasma Deposition (MEPD) system deposits a 1 micron layer of magnetic property enhancement material (may employ different elements) on the surface of the target device. This enhances the effects of the TSA activities.
Target acquisition by the PAAP automatically triggers the TSA to begin startup actions based upon type of device, device momentum and mass, time-to-target and alignment processing type. Device data download of mission specifics is derived from either optical beam-ride technology using the central axis HDLA and/or electronic telemetry. This information is passed to the TSA to develop TTFF parameters. Major components of the PAAP consist of the HDLA, the VLAPFM and the TSNA. Power is generated via a combination of technologies using solar, SNAP Thermonic converters, Standard Orbital Atomic Reactor and/or fusion tap from the SEFGs.
Design Specifics - Request only
Time-Space Aperture (TSA)
Function
The Time-Space Aperture (TSA) is the device used to modify the time continuum and inject target devices through the time/space event envelope.
Design Overview
Basic TSA design features include the Time-Space Torroidal Focal Field (TTFF) , the Synchronous Event Field Generators (SEFG) and the Standard Orbital Atomic Reactor (SOAR). Once the target device leaves the PAAP, the TSA structure allows for the target device to be captured for a period of time and exposed to the TTFF being generated from the synchronous event field generators. Depending upon target and mission specifics, the TTFF is modified to accomplish required affects. The TSA design draws upon magnetic field flux density, induction, Poynting Vectoring effects, De Broglie wavelength theorems, Planks constant and Lorentz Contraction functions in development of the time-space focal field.
Electromagnetic waves under certain circumstances have properties indistinguishable from those of matter. The application of quantum mechanics allows us to extrapolate terms associated with the momentum of a photon and apply (using relativistic formula) to the properties of matter based on Planks constant, known mass and velocity and other specifics of the target device. Given information gathered from these and other sources of data, a localized time gradient in the scalar gravitational potential is superimposed across the symmetric gravitational potential already present from the vehicle's mass. This induced effect is represented by a magnitude and is localized by a Gaussian distribution over the distance and centered at the target device. With a know circumference of the TSA, calculations can deduce orbital frequencies necessary to impart the required energy input from the SEFGs to develop the magnetic field densities and direction of rotation thereof to develop the time event envelope. These gravinometric and time alterations are applied to the target device in a manner similar to magnetic field applications associated with core solenoid functionalities since the target device was initial ‘blown' with a plasma arc of magnetic enhancing material.
Design Specifics - Request Only
Operation Overview - Request Only
Drawings and Renditions - Request Only
