Space infrastructure · Denver, Colorado

Most things in space tumble. Almost nothing can catch them.

Delta Infinite builds a two-part reactive foam that stops the spin and leaves behind a standard grapple point — so capture systems can service or remove objects they currently cannot approach.

Delta Infinite

The problem

Real targets often spin faster than rigid capture can handle.

Rigid capture systems need a target that’s nearly still — they top out around three to five degrees per second. Recently failed satellites typically tumble at three to eight degrees per second. Long-derelict objects reach tens of degrees per second, and a target’s rate is neither knowable in advance nor stable.

It isn’t just the grapple.

The ceiling isn’t set by the capture mechanism alone. At contact, a tumbling target’s angular momentum transfers into the capturing spacecraft, and its attitude determination and control system (ADCS) — the reaction wheels and thrusters that keep it pointed — has to absorb it. Reaction wheels hold a finite amount of momentum. Against a heavy, fast-tumbling target they saturate, and the spacecraft either burns propellant to recover or loses control of its own orientation.

Our system doesn’t match the spin. It removes it.

01 · DEPLOY

Foam on target

A two-part reactive foam is deployed onto the target.

02 · EXPAND & CURE

The tumble slows

It expands and cures in vacuum, slowing the tumble by redistributing mass and dissipating rotational energy.

03 · GRIP

A standard surface

What’s left is a stabilized object with a standardized surface any capture system can grip.

Why it matters

Capture comes first.

Servicing, debris removal, and relocation all start the same way: taking hold of an object that was never designed to be caught. Most of what’s in orbit has no grapple fixture and no docking interface. Until an object is stable, nothing else can happen to it.

The same step sits at the center of asteroid resources.

~8×
lower cost per kilogram than launching the same mass from Earth, for a first asteroid-return mission
~20×
lower on repeat missions

A 2012 feasibility study by the Keck Institute for Space Studies at Caltech estimated that returning a small near-Earth asteroid could deliver mass to high lunar orbit at roughly one-eighth the per-kilogram cost of launching it from Earth, and about one-twentieth on repeat missions. That architecture depends on capturing and de-spinning a tumbling, non-cooperative body, autonomously, in deep space.

NASA carried the concept forward as the Asteroid Redirect Mission and cancelled it in 2017, after its cost estimates grew. We’re doing this to get to that: prove the capture layer in Earth orbit, where the need is immediate and the market already exists, then carry it outward. Asteroid resources are the long-horizon destination.

Source: Brophy et al., Asteroid Retrieval Feasibility Study, Keck Institute for Space Studies, 2012.

Where we are

TRL 3, closing on TRL 4.

2024 · Tested
First successful vacuum foam-deployment test completed.
Modeled
Capture dynamics modeled against real physics.
Documented
A thermal-vacuum validation campaign written to formal standard.

On record

WarpWare

WarpWare — executed services agreement. Coupled physics modeling, simulation, and capture dynamics characterization.

KMI SPACE

KMI Space — conditional, non-binding letter of intent, contingent on TRL 4 validation.

AFRL

Confirmed technical point of contact at AFRL with Phase I proposal support offered.

Timeline

Milestones

  1. 2017

    The gap

    NASA cancels its Asteroid Redirect Mission after cost estimates grow. Affordable capture of a tumbling, uncooperative object remains an open problem.

  2. 2018

    Foam

    A space-rated foam as the interface between a capture system and a tumbling, uncooperative target. The company gets its name: Delta Infinite — infinite change.

  3. 2019–21

    Theory

    Foam behavior under vacuum, and the framework for a deployable foam capture interface.

  4. 2022

    Founded

    Company formation with support from the Santa Cruz SBDC and the Entrepreneurs’ Law Clinic at Santa Clara University.

  5. 2023

    The team forms

    Jim Cochran-Miller joins as Engineering Lead. Dr. Michael Browne joins as Science Lead.

  6. 2024

    First vacuum test

    The team builds a vacuum chamber, holds stable vacuum over 24 hours, and completes the first successful vacuum foam-deployment test. Delta Infinite LLC is formed and the company relocates to Colorado.

  7. 2025

    Federal readiness

    Government-compliant indirect rate structure in place. NASA SBIR Phase I and Colorado OEDIT applications prepared. Invited to pitch to space-resources investors at Colorado School of Mines.

  8. 2026

    Third-party validation

    • AprKMI Space — conditional, non-binding letter of intent, contingent on TRL 4 validation.
    • MayWarpWare — executed services agreement.
    • MayThermal-vacuum validation campaign written to formal standard.
    • JunConfirmed technical point of contact at AFRL with Phase I proposal support offered.
  9. Now

    Closing on TRL 4

    The validation campaign is scoped, documented, and gated on funding. Bootstrapped to this point without external capital. We’re looking for investors, capture and servicing partners, and program offices to take it through TRL 4.

Team

Who’s building it

Jim and Michael contribute to Delta Infinite at no cost to the company at this stage, converting to funded full-time roles at seed.

Kai Cahlil
Kai Cahlil
Founder & CEO

Working toward asteroid resource capture since 2012; founded Delta Infinite in 2022. Leads strategy, partnerships, and funding, and set up the company’s federal contracting foundation.

Jim Cochran-Miller
Jim Cochran-Miller
Engineering Lead

Builds the test environment: the vacuum chamber the foam is tested in, now in its third revision.

Full bio

Jim takes concepts through testing into practical application. Ten-plus years managing the design and construction of district energy and energy conservation systems — hydronic, controls, telecommunications, electrical, and manufacturing process systems — for clients including Apple, the U.S. Navy, the U.S. Air Force, UC Berkeley, and CSU Fresno, on projects ranging from $10M to $200M. Aeronautical and mechanical engineering, Clarkson University.

At Delta Infinite he builds the test environment. The vacuum chamber the foam is tested in is his, now in its third revision, and he leads the expansion into thermal cycling and UV exposure. In his words: “I love being able to identify a problem, break it into solvable pieces, and then tackle those pieces one at a time.”

Dr. Michael Browne
Dr. Michael Browne
Science Lead

Leads foam chemistry, cure characterization, and materials testing.

Full bio

PhD in analytical and biophysical chemistry from University of the Pacific; BS in pharmaceutical chemistry from UC Davis. Managed the University of the Pacific mass spectrometry facility, with instrumentation depth across LC-MS/MS, GC-MS/MS, pyrolysis GC-MS, DART-MS, and HRMS. Published in the International Journal of Mass Spectrometry, Biopolymers, and the Journal of Physical Organic Chemistry. Previously at Chevron Energy Technology. Currently a PK/PD bioanalytics scientist at Firefly Bio.

His work identifies and solves the two problems gating everything else: vacuum bubble collapse and cure kinetics. He has demonstrated mitigation of the former through bulking agents, and defines the analytical instrumentation strategy for the thermal-vacuum campaign.

Thornelia, a Mammillaria spinosissima cactus
Thornelia
Growth Lead

As a Mammillaria spinosissima, Thornelia champions patient, resilient growth, thriving under harsh conditions and reminding the team that even the most ambitious missions begin with strong roots.

Get in touch

Start a conversation.

Investors, capture and servicing operators, program offices, and researchers working on non-cooperative capture: we’d like to hear from you.

kai@delta-infinite.com · Denver, Colorado