Abstract

The Caldwell Integrated Space Resilience Architecture (CISRA) is a conceptual open-hardware framework intended to organize previously disclosed Technical Disclosure Commons (TDC) inventions related to launch systems, orbital debris mitigation, communications, thermal management, environmental control and life support, energy systems, and long-duration space operations.

The architecture seeks to address several long-term challenges associated with humanity's expansion into space:

• launch cost • orbital congestion • debris accumulation • thermal management • communications capacity • life-support sustainability • resource efficiency

The purpose of this disclosure is to establish a conceptual framework showing how multiple previously disclosed inventions may interact within a larger space-operating ecosystem.

IMPORTANT NOTE REGARDING PRIOR DISCLOSURES

Readers are encouraged to review the original Technical Disclosure Commons (TDC) publications for detailed subsystem descriptions, assumptions, limitations, engineering considerations, and theoretical foundations.

The following previously disclosed inventions contribute conceptually to the CISRA framework.

Launch and Space Access

• STARLIFT V3: A MULTI-LAYER ELECTROMAGNETIC–TETHER LAUNCH ARCHITECTURE

Orbital Sustainability and Debris Mitigation

• Contactless Orbital Debris Shepherd (CODS)

Communications

• Structured Multimode Optical Communication System With Engineered Channel Mixing and DSP-Based Signal Recovery (GCI-286 “Ariadne’s Braid”)

Thermal Management

• GCI #271 – Active Orbitronic Heat-Pump Substrate (v2) • GCI #278 — Helium-Sparing Multi-Stage Vortex Cryocooling Stack with Modular Geometry and Arachne Thermal Interface • GCI #75: Thermo-Orbitronic Testbed Using Chiral-Phonon-Induced Orbital Currents in Quartz

Space Life Support and Environmental Systems

• Sentinel Passive Vortex Space Toilet Separator (SPVTS-1) • Sentinel-Vortex Bio-Processor v4.0: Passive, Fanless Urine-Air Separator for Microgravity ECLSS

Infrastructure and Monitoring

• Arachne v8.7: Multi-Modal Energy-Harvesting Smart-Skin with Hierarchical Fractal Morphology, Distributed MIS Interface, and Integrated Structural-Health Monitoring • The GCI Vortex Spine: Integrated Vortex-Induced Energy Platform Using Arachne v8.7 Smart-Skin, Resonance-Adaptive Logic, and Gyroid-Lattice Structural Core

MISSION

To improve the sustainability, efficiency, resilience, and affordability of future space operations through integrated engineering architectures.

DESIGN PHILOSOPHY

Long-term space development depends on solving multiple interconnected challenges simultaneously:

  1. Affordable access

  2. Sustainable orbital operations

  3. Reliable communications

  4. Efficient thermal control

  5. Resource recovery

  6. Life-support resilience

CISRA seeks to address these challenges as a unified system.

MODULE 1 – SPACE ACCESS PLATFORM

Derived Conceptually From

• STARLIFT V3: A MULTI-LAYER ELECTROMAGNETIC–TETHER LAUNCH ARCHITECTURE

Creative Commons License

Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 License.

Download

Share

COinS