Abstract
O'Neill and Kolm's November 1980 Acta Astronautica paper "High acceleration mass drivers" (7(11): 1229-1238) is the canonical peer-reviewed primary publication on the mass driver concept from the foundational period. The paper presents the technical case for high-acceleration (>1000 g) operation as the path to compact, low-mass lunar launchers — extending the Mass Driver 1 (1976, 33 g, $2000 budget, 40 m/s) and Mass Driver 2 (1978-1982, 500 g design / 5000 m/s² achieved, 112 m/s final velocity) program to a Mass Driver 3 envelope. The paper is the formal academic-venue companion to the NASA SP-428 Mass Drivers I/II/III chapter and to the SSI / Princeton AIAA Symposium proceedings. PDF not directly accessible via WebFetch in this session; citation and key parameters confirmed via O'Neill Wikipedia, NASA SP-428 derivative content, and L5 News Kolm 1980 update.
Key claims
- primary-publication: O'Neill & Kolm, "High acceleration mass drivers," Acta Astronautica 7(11): 1229-1238, November 1980 — peer-reviewed primary source.
- companion-publications: O'Neill, Driggers & O'Leary (1980) "New Routes to Manufacturing in Space" Astronautics & Aeronautics 18(10): 46-51; O'Neill (1978) "The Low (Profile) Road to Space Manufacturing" Astronautics & Aeronautics 16(3): 18-32; O'Neill (1976) "Engineering a Space Manufacturing Center" Astronautics & Aeronautics 14: 20-28.
- mass-driver-1: "Constructed in 1976 at MIT with Henry H. Kolm. Eight-foot length delivering 33 g-force acceleration. Public debut at Princeton's Chadwin Hall."
- mass-driver-2: "Operate in an evacuated, four-inch caliber tube at an acceleration of 500 gee, with a superconducting bucket and an oscillating, push-pull coil system" (Kolm 1980 derivative). Achieved 5000 m/s² acceleration, 112 m/s final velocity by 1982.
- mass-driver-3-envelope: "Later models, supported by SSI funding, achieved 1,800 g-force acceleration, sufficient for launching lunar material via a 520-foot-long device."
- canonical-lunar-spec: "A conservative design using existing technology could theoretically deliver 600,000 tons a year to L-5...at a cost of about $1 per pound, assuming only ten years of operation."
Reviewer notes
The Acta Astronautica 1980 paper itself is paywalled / not fetched in this session; the bibliographic anchor is established but the verbatim text of the paper's results is not in this extract. The "$1 per pound" headline comes from Kolm's L5 News (1980) update, which references the same NASA / MIT / Princeton group's work and the same $3.137B / 600 kt/yr / 10-year ops scenario as the NASA SP-428 chapter. This is a single co-author network (O'Neill, Kolm, Mongeau, Snow, Fine, Williams) producing peer-reviewed papers, NASA technical reports, and trade press in parallel. Tier S as a peer-reviewed primary publication; recommend a future iteration fetch the full PDF (university library or SSI archive). All numeric claims in the L5 News and SP-428 derivatives match each other internally, suggesting they are not independent triangulation but rather one common source presented in multiple venues. Note: Mass Driver 1's 33 g figure is consistent across sources; the 1800 g claim for later models is contemporaneous-design (paper proposal) rather than achieved-prototype.