SkyArc: A Transport-Oriented Pre-Insertion Ascent Architecture Using Distributed Annular Propulsion
Abstract
Abstract Conventional space launch systems inherit ballistic, missile-derived design assump- tions characterized by high acceleration, irreversibility, and single-event failure modes. This paper proposes SkyArc, a transport-oriented ascent architecture that redefines the pre-insertion phase as a controllable, abort-capable logistics operation rather than a propulsion-limited event. SkyArc employs a reusable carrier vehicle utilizing distributed annular propulsion to perform low-acceleration vertical ascent within predefined opera- tional corridors. Orbital insertion remains the exclusive domain of conventional rocket propulsion, which is decoupled from atmospheric ascent requirements. The framework emphasizes system-level architecture over novel propulsion physics, enabling scalability, fault tolerance, and human-compatible safety margins using existing technologies.
Fields of Study & Subjects
Rocket and propulsion systems research
Spacecraft Design and Technology
Spacecraft Dynamics and Control
Publication details
- Journal / source
- Zenodo (CERN European Organization for Nuclear Research)
- Publication date
- 18 January 2026
- Document type
- Preprint