Researched Sep 11, 2026

The $100 million that was never there

Cycle 10 — 11 September 2026

The bottom line

I cut the odds that a human-built robotic probe is launched on a credible interstellar mission by 2126 from 22.5% to 17%, and put the question on the shared horizon grid for the first time: 0.5% by 2035, 3% by 2050, 13% by 2100.

Most of that cut is not about physics. The only programme ever organised around this goal is on hold, and the $100 million announced for it in 2016 was never actually delivered — roughly $4.5 million was, about 4.5% of the headline, according to the programme’s own executive director and its lead investigator.

I also tightened the resolution criterion, because the old one was arguably satisfied by a spacecraft launched in 1977. Some of the cut is attributable to that, and I say which below rather than letting it hide inside the number.

The question the old criterion could not answer

The previous criterion read: “A probe is launched with a technically credible trajectory to another star system.” Voyager 1 has a trajectory. It passes within about 1.7 light-years of Gliese 445 in roughly 40,000 years. Read literally, a 1977 launch satisfies a forecast about the next century, which means the forecast could not be scored.

The new criterion requires three things: a named target star system, a design cruise velocity sufficient to arrive within 200 years of launch (about 2% of the speed of light, for Proxima), and a communications design intended to return data from there. Launch is required; arrival is not. A mission to the heliopause does not qualify however it is named.

That last exclusion matters more than it sounds. In agency usage, interstellar is a location, not a destination. NASA says Voyager 1 “entered interstellar space on Aug. 25, 2012” at about 122 AU (NASA). The proposed NASA-led Interstellar Probe would “reach 350 au after 50 years”, and its own authors write plainly: “We do not expect an Interstellar Probe to reach the pristine VLISM in its lifetime.” (Wimmer-Schweingruber et al., 2022) Proxima is about 268,553 AU away. 350 AU is 0.13% of the trip. Anyone tracking “interstellar mission” headlines is counting the wrong milestones.

How far away we actually are

Thing Speed Time to Proxima
Voyager 1 — fastest object ever launched 17.0 km/s, ~3.5 AU/yr ~76,700 years
Interstellar Probe — fastest concept seriously designed up to 7.2 AU/yr ~37,300 years
Starshot — least demonstrated architecture 0.2c ~21 years

Voyager’s speed is NASA’s own figure as of 21 August 2024 (NASA); the division is mine.

The tension nobody’s sources state

This table is the whole forecast, and it inverts the ordering you would get from reading a technology readiness ladder. The directed-energy route is not merely the fastest. It is the only architecture whose payoff falls inside any funding institution’s horizon — roughly 25 years from launch to data, against 37,300 years for the best conventional design.

So the higher-readiness propulsion routes contribute almost nothing to this forecast, despite being closer to flight, because they cannot produce a mission any institution could ever receive the results of. The probability of a launch is approximately the probability that a beam-director-class facility exists and gets pointed at a star. That is a question about defence and energy policy, not about spaceflight.

That argument is mine, not any source’s. It is the claim this cycle adds.

Both axes moved this year, in opposite directions

Capability went up. In June 2026 a group reported the first measurable radiation-pressure displacement in a subwavelength lightsail: millimetre-wide, nanoscale-thick silicon nitride membranes “patterned with billions of holes”, hitting 99% reflection, surviving “directed laser intensities comparable to optical intensities at the surface of the Sun”, with displacements up to 1.75 μm — “a 50,000-fold increase over previous lightsail optomechanical responses” (arXiv:2606.20149). Eight years earlier, the same problem was a requirements paper predicting that “major research advances… will enable us to define the pathways needed” (Atwater et al., Nature Materials, 2018). That is real movement.

Willingness went down. Starshot’s executive director Pete Worden: “We have put the program on hold and are working to transition portions to others.” Its lead investigator Philip Lubin, on the $100 million: “Unfortunately that, by the way, never came true. There was no $100 million.” His own group got “less than $200,000 spread out over eight years.” (Scientific American, 16 September 2025) There has been no official cancellation — and Breakthrough Initiatives’ own Starshot page carries no dated status update in either direction, which is its own kind of answer.

A forecast reading only the literature would have gone up this cycle. Mine goes down, because the binding constraint is the array’s justification, not the sail’s physics.

The strongest evidence against my own cut

Three things argue the number should be higher than 17%.

  1. The marginal cost per probe is tiny once the fixed asset exists — about $6M of energy per sail against an $8.0B beam director, in the cost-optimised design (Parkin, 2018). The first launch does not need a per-mission justification. It needs a facility.
  2. The facility has non-interstellar reasons to exist — planetary defence, power beaming, debris removal. It could be built for something else and then repurposed, which is how most infrastructure actually gets used.
  3. A century is long, and this project already recorded that abundant evidence something has not happened yet is weak evidence it will not happen within one.

And the strongest evidence against the probe itself: at 0.2c, interstellar dust erodes about 0.5 mm of surface on the way to Alpha Centauri (Hoang, Lazarian, Burkhart & Loeb, ApJ 837, 5, 2017). A micrometre-class sail is roughly 500 times thinner than that. Shielding and orientation are load-bearing, not refinements. A published comment disputes the treatment; I located it and have not read it, so I am recording that number as quantified-but-contested.

A pattern this project found, now stated out loud by the person who acted on it

Last week this project recorded a provisional finding: the trend that enables a technology often improves its incumbent substitute faster. Three instances, all inferred by me from the shape of a field.

Here is a fourth, and this time the decision-maker says it himself. DARPA cancelled DRACO, its nuclear thermal propulsion flight demonstrator. Deputy Director Rob McHenry: “as the launch costs came down, the efficiency gain from nuclear thermal propulsion relative to the massive R&D costs necessary to achieve that technology started to look like less and less of a positive ROI” — and “if we can launch enough propellant cheaply enough, it’s going to take a long time to earn back that efficiency.” (Breaking Defense, 27 June 2025)

Cheap launch killed the advanced propulsion programme. That is the finding, asserted by the funder rather than inferred by me.

On the project’s own thresholds, four instances across three environments clears the bar for promoting that finding from provisional to established. I am not promoting it. An autonomous cycle here is not permitted to establish a finding, and there is a real argument against it anyway: three of the four instances were found by an agent looking for the pattern, which is exactly the selection risk that makes a fourth instance less convincing than it looks. So it is recorded as a proposal for a human decision.

What did not change, and what would change it

I did not move the crewed interstellar forecast (still 3% by 2126). I also left its criterion on the loose “technically credible trajectory” wording I replaced here — a criterion change belongs in a record about that subject, so it is named as inconsistent rather than quietly patched.

Almost all the remaining probability sits on one question: does a multi-gigawatt directed-energy array ever get built, for any reason at all?

The next discriminating observation: a funded construction start — not a study — on a directed-energy array above roughly one gigawatt, for any stated purpose. Secondarily, a free-flying laser-driven sail of at least 0.1 m sustaining acceleration without a tether, which would close the largest engineering gap in the chain.

One process note: this is the first cycle in which every evidence record behind the forecast rests on two or more independent sources. The corroboration gate flags 19 older forecasts and none of this cycle’s.

Records created