ONE CATALOG
A single picture that keeps covariance for every object, from missile tracks to asteroids, on open CCSDS and MPC standards.
One layered architecture against three kinds of threat: asteroids and comets, a crowded and contested orbital environment, and missiles that pass through space. The missions share sensors, a single track picture, communications and logistics. They differ in timeline, decision authority and effectors.
The same infrared satellite that watches for missile launches also sees meteors entering the atmosphere. The same telescopes that maintain the orbital catalog catch asteroids on close approach. So the architecture is built around one track picture.
Survey for near-Earth asteroids and comets, characterize them, and deflect with a kinetic impactor, gravity tractor or, as a last resort, a standoff burst.
EXPLORE THE MISSION →One catalog with covariance, conjunction assessment, characterization, servicing and debris removal, from LEO to cislunar space.
EXPLORE THE MISSION →Space-based warning and birth-to-death tracking, plus open trade studies of interceptor layers and their absentee ratio.
EXPLORE THE MISSION →Each layer starts from infrastructure that already operates and adds the pieces that close the gaps.
L0 · Ground and sea | Reuse: Space Fence, the Space Surveillance Network, Rubin/LSST, ATLAS, Catalina, Goldstone, commercial SSA networks, ground and sea interceptors Add: Deep-space radar to replace Arecibo; distributed GEO and cislunar telescopes; optical ground terminals |
|---|---|
L1 · Low Earth orbit | Reuse: Proliferated transport and infrared tracking layers; commercial meshes as hosts Add: Continuous custody of hypersonic tracks; SSA sensors looking up from LEO; inspectors; an optional interceptor layer, subject to trade |
L2 · MEO / GEO / HEO | Reuse: SBIRS and Next-Gen OPIR; GEO neighbourhood watch; commercial life-extension servicers Add: Maneuverable GEO patrol satellites; refueling depots; debris-removal tugs; polar HEO warning |
L3 · Cislunar | Reuse: Little dedicated capability today Add: SSA sentinels at Earth–Moon L1/L2; relay and timing node; parking orbit for a ready asteroid interceptor |
L4 · Heliocentric | Reuse: NEO Surveyor; the DART and Hera results Add: IR survey inside Earth's orbit near Venus; rapid reconnaissance flyby spacecraft; the deflection ladder |
Every mission runs the same chain. What changes is how long each step is allowed to take, and who decides.
A single picture that keeps covariance for every object, from missile tracks to asteroids, on open CCSDS and MPC standards.
Seconds and pre-authorized for missiles; operator-in-the-loop for orbit; deliberative and international for asteroids.
Crosslinks between LEO satellites, relays in GEO and cislunar space, and a resilient ground network.
No destructive tests in orbit, a disposal plan for every spacecraft, and every design screened for collision risk.
The first phase builds nothing in orbit. It connects what exists and builds the tools that size everything after it.
Fuse existing sensors into one track picture and digital twin; build the open trade-study toolchain.
Expand LEO infrared tracking; GEO and cislunar SSA sentinels; NEO Surveyor operations; deep-space radar.
A ready asteroid interceptor; servicing and debris removal; an evidence-based decision on interceptor layers.
A Venus-region infrared survey, a cislunar relay, and the full deflection ladder.
The same rule as every Aerospace Superintelligence program.
An architecture is a hypothesis until a reproducible trade study says otherwise.
Every number on these pages is a planning estimate from public sources. The program's job is to replace each one with a traceable result from open analysis tools: stated assumptions, the tool version, the inputs, and the output. The work uses public, unclassified sources only.