Quantum Light Engine: A Novel Propellantless Photonic Propulsion Concept
Abstract
We present a novel quantum light propulsion system utilizing a Penrose-tiled blackbody diode doped with neodymium, optically pumped by high-power lasers to generate a coherent Bose photon gas. This low-entropy quantum light is harvested and injected into multiple nested perfectly reflective toroidal waveguides, forming circulating photon rings with substantial angular momentum and energy density. The combined energy-momentum distribution of these nested rings induces localized spacetime curvature and frame-dragging effects, modeled within the framework of general relativity. These relativistic phenomena produce measurable time dilation and gravitational frequency shifts, enabling phase manipulation of the confined photon fields. Controlled asymmetric photon emission from the nested system converts photon momentum into directed thrust, providing a propellantless propulsion mechanism. This integrated approach bridges quantum optics and gravitational physics, suggesting a scalable pathway for advanced photonic propulsion leveraging engineered spacetime dynamics.
Theoretical Framework and Key Equations
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Quantum Light Generation in Penrose-Tiled Blackbody Diode
A Penrose-tiled blackbody diode doped with neodymium ions is optically pumped by high-power lasers, producing a Bose-Einstein photon gas with coherent quantum light:
Energy E = h × f = h × c / λ
Momentum p = E / c = h / λ
where h = Planck’s constant, f = photon frequency, c = speed of light, λ = wavelength. -
Injection into Nested Toroidal Waveguides
Quantum light is harvested and injected into multiple nested perfectly reflective toroidal cavities at radii R_i, generating circulating photon rings. The combined energy-momentum tensor is:
T^(μν)(x) = sum over i=1 to N of [E_i / (2 π R_i)] × delta(r - R_i) × delta(z) × u^μ u^ν
where E_i is photon energy in the i-th toroid, u^μ is the photon four-velocity. -
Spacetime Curvature from Photon Rings
The nested photon rings act as sources in Einstein’s field equations, curving spacetime:
G_(μν) = (8 π G / c^4) × T_(μν)
where G_(μν) is the Einstein tensor, G is the gravitational constant. -
Time Dilation within Toroids
Each toroid’s gravitational potential
Φ_i = G × E_i / R_i
induces time dilation:
dτ/dt = sqrt(1 - 2 Φ_i / c^2)
where τ is proper time and t is coordinate time. -
Frame Dragging Due to Angular Momentum
The angular momentum of the photon ring
J_i = R_i × E_i / c
causes frame dragging with angular velocity
Ω_i ≈ G × J_i / (c^2 × R_i^3) = G × E_i / (c^3 × R_i^2). -
Gravitational Frequency Shift
Photons escaping the gravitational well experience blueshift:
f_obs = f_emit × (1 - ΔΦ / c^2)^(-1/2). -
Net Thrust from Asymmetric Photon Emission
Controlled asymmetry in photon leakage produces thrust:
F = dp/dt = (1 / c) × dE/dt. -
Total Stress-Energy Tensor of Nested Toroids
The entire nested system’s energy-momentum is:
T_total^(μν) = sum over i=1 to N of [E_i / (2 π R_i)] × delta(r - R_i) × delta(z) × u^μ u^ν,
amplifying gravitational and frame dragging effects.
Conclusion
This study proposes a novel propellantless propulsion system based on a quantum light engine that integrates a Penrose-tiled blackbody diode with nested, perfectly reflective toroidal waveguides. Coherent Bose photon gases generated within the diode are injected into these toroids, where they circulate as quantum light rings. The nested configuration of the toroids enhances the combined energy density and angular momentum, inducing localized spacetime curvature, time dilation, and frame-dragging effects as described by general relativity. By carefully controlling asymmetric photon emission from this relativistic light environment, the system can convert confined photon momentum into directed thrust—without the use of conventional propellant. This concept bridges quantum optics and gravitational engineering, offering a promising framework for scalable, propellantless space propulsion. Further modeling and validation will be essential to realize its full potential for advanced aerospace applications.
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