Project Timber Wind (1987-1991) and its successor Space Nuclear Thermal Propulsion (SNTP) program (1991-1994) were classified Department of Defense efforts to field an ultra-lightweight particle-bed nuclear-thermal rocket for missile-defense payloads.1
SDIO spent roughly $139 million before transferring the work to the Air Force, which added about $60 million — total outlays approached $200 million when headquarters halted SNTP in January 1994.1
Four phases — concept definition, reactor and fuel development, ground-test planning, and cancellation — are documented in audits, congressional testimony, and the 1995 Phillips Laboratory final report.2 Earlier congressional and Department of Energy reviews traced the concept's heritage and risk posture.34
Timeline of Major Events
Technical Architecture
Particle-Bed Reactor Core
Fine uranium-carbide particles sintered into porous spheres, coated for hydrogen compatibility, and packed in a zirconium-niobium matrix yielded outlet temperatures near 2700 K.72 The target engine produced 25 000 lbf thrust at a specific impulse close to 1000 s while keeping dry mass near 1.65 tonnes—about one-third of a comparable NERVA stage.2
Support Systems
Turbopump, attitude-control, and nozzle hardware were contracted to Hercules Aerospace, AiResearch, and Grumman; each used carbon-carbon composites to endure hot hydrogen flow.212 Propellant-cooled tungsten and lithium-hydride shielding designed at Sandia protected cryogenic tanks and met human-rating thresholds.
Planned Test Series
- Fuel-element irradiation loops at Brookhaven and the Idaho National Engineering Laboratory.
- Hot-hydrogen flow tests of full-scale fuel elements at Arnold Engineering Development Center.
- Prototype engine firings (1 000 s) inside a vacuum duct at the Nevada Test Site's Saddle Mountain complex.713
Program Organization and Key Personnel
Oversight, Classification, and Security Disputes
TIMBER WIND functioned as an unacknowledged special-access program; the Inspector-General concluded the status lacked merit after the Air Force released reactor data.6 GAO warned that undefined mission requirements and the $400 million ground-test infrastructure estimate posed unacceptable cost risk.17 External pressure from Aftergood's FOIA campaign and the Nozette espionage case maintained scrutiny and eroded institutional support.1114
Cancellation Drivers and Legacy
Post-Cold-War budget cuts removed the missile-defense requirement for a particle-bed upper stage, and NASA judged that existing NERVA-class hardware could serve Mars missions more cheaply.115 The 1993 facility study and environmental review showed that no U.S. site could test a full reactor without major new construction, pushing life-cycle cost beyond $1 billion.78 Although the prototype never fired, materials data, fuel-coating techniques, and carbon-carbon structures informed later NASA Mars-vehicle analyses and current DARPA/NASA DRACO plans.215 The IG audit and Aftergood's activism are now cited in classification-policy courses as examples of SAP justification pitfalls.61116
References
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GAO, Space Nuclear Propulsion: History, Cost, and Status of Programs T-NSIAD-93-2. https://www.gao.gov/assets/t-nsiad-93-2.pdf ↩ ↩2 ↩3 ↩4 ↩5 ↩6 ↩7 ↩8
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Phillips Laboratory, Space Nuclear Thermal Propulsion Program Final Report PL-TR-95-1064. https://www.osti.gov/biblio/273151 ↩ ↩2 ↩3 ↩4 ↩5 ↩6 ↩7 ↩8
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Congressional Research Service, RL 31347 Nuclear Propulsion (1991). https://crsreports.congress.gov/product/pdf/RL/31347 ↩
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Department of Energy, Space Nuclear Propulsion Program History (1995). https://www.energy.gov/sites/default/files/2021-02/Space_Nuclear_Propulsion_History.pdf ↩
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Magnetic Glide Technologies, James R. Powell biography. https://www.magneticglide.com/about-us.html ↩ ↩2
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DoD Inspector-General Audit Report 93-033, TIMBER WIND Special Access Program. https://sgp.fas.org/othergov/dod/tw.pdf ↩ ↩2 ↩3 ↩4 ↩5 ↩6
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NASA TM-105708, Space Nuclear Thermal Propulsion Test Facilities Sub-panel Final Report. https://ntrs.nasa.gov/api/citations/19930015916/downloads/19930015916.pdf ↩ ↩2 ↩3 ↩4 ↩5
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USAF, Final Environmental Impact Statement—Space Nuclear Thermal Propulsion Program. https://ntrs.nasa.gov/api/citations/20140008803/downloads/20140008803.pdf ↩ ↩2
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NRC docket material referencing the SNTP EIS. https://www.nrc.gov/docs/ML0222/ML022270728.pdf ↩
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Archive.org copy of PL-TR-95-1064. https://archive.org/details/a305996 ↩
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Federation of American Scientists, Nozette and Nuclear Rocketry. https://fas.org/publication/nozette/ ↩ ↩2 ↩3 ↩4 ↩5
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Air Force Research Laboratory hot-hydrogen test fact sheet. https://www.afrl.af.mil/About/Fact-Sheets/Fact-Sheet-Display/Article/2282103/ ↩
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INL Digital Library reference citing the SNTP EIS. https://inldigitallibrary.inl.gov/sites/sti/sti/4886666.pdf ↩
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YNet News, US Scientist Indicted for Espionage, 2009. https://www.ynetnews.com/articles/0,7340,L-3794208,00.html ↩ ↩2
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NASA Space Nuclear Propulsion Office Report, 1994. https://www.nasa.gov/sites/default/files/atoms/files/nasa_space_nuclear_propulsion_1994.pdf ↩ ↩2
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New Space Economy, Rise and Fall of Project Timber Wind (2024). https://newspaceeconomy.ca/2024/02/16/the-rise-and-fall-of-project-timberwind-americas-secret-nuclear-rocket-program/ ↩