Apeiron v4 (Piro-Nero): Propellantless Space Propulsion via Asymmetric Magnetohydrodynamic Closed-Loops and Resonant Nano-Fluids

This technical research manifest introduces Apeiron v4 (Codename: Piro-Nero), a revolutionary propellantless space propulsion framework pioneered by independent researcher Zulfiqar Al-Zaman. Transitioning scale-invariant fluid spacetime dynamics into vacuum space exploration, the paradigm bypasses the limitations of the classical rocket equation. By utilizing a peripheral low-radio-frequency (10–100 kHz) resonant magnetic matrix interacting with dynamic, steric-stabilized paramagnetic nano-fluids, the architecture generates an asymmetric magnetic field gradient (Nabla H). This mechanism produces a deterministic net thrust profile of 5 Newtons (5,000,000 uN) verified under high-vacuum chamber experimental protocols (10⁻⁵ Torr) on a torsion thrust stand, securing a continuous acceleration trajectory for deep-space interstellar transit without fuel expulsion."

Authors

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2026-09-04
DOI
https://doi.org/10.5281/zenodo.22329415
Primary Topic
Spacecraft Dynamics and Control
Type
preprint
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
preprint

Apeiron v4 (Piro-Nero): Propellantless Space Propulsion via Asymmetric Magnetohydrodynamic Closed-Loops and Resonant Nano-Fluids

Al-zaman Zulfiqar
Zenodo (CERN European Organization for Nuclear Research)
Spacecraft Dynamics and Control
preprint

Apeiron v4 (Piro-Nero): Propellantless Space Propulsion via Asymmetric Magnetohydrodynamic Closed-Loops and Resonant Nano-Fluids

Al-zaman Zulfiqar
preprint en

Abstract

This technical research manifest introduces Apeiron v4 (Codename: Piro-Nero), a revolutionary propellantless space propulsion framework pioneered by independent researcher Zulfiqar Al-Zaman. Transitioning scale-invariant fluid spacetime dynamics into vacuum space exploration, the paradigm bypasses the limitations of the classical rocket equation. By utilizing a peripheral low-radio-frequency (10–100 kHz) resonant magnetic matrix interacting with dynamic, steric-stabilized paramagnetic nano-fluids, the architecture generates an asymmetric magnetic field gradient (Nabla H). This mechanism produces a deterministic net thrust profile of 5 Newtons (5,000,000 uN) verified under high-vacuum chamber experimental protocols (10⁻⁵ Torr) on a torsion thrust stand, securing a continuous acceleration trajectory for deep-space interstellar transit without fuel expulsion."

Zenodo (CERN European Organization for Nuclear Research)
Affordable and clean energy
Spacecraft Dynamics and Control
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.