DOW-UAP-D126, AAWSAP DIRD, Advanced Nuclear Propulsion for Manned Deep Space Missions, March 2010
Department of War · 3/11/10 · Las Vegas, Nevada · Document
DOW-UAP-D126, AAWSAP DIRD, Advanced Nuclear Propulsion for Manned Deep Space Missions, March 2010 is indexed as a Department of War record with incident date 3/11/10 and location Las Vegas, Nevada. This document is a Defense Intelligence Reference Document (DIRD), a technical reference format used by the Defense Intelligence Agency (DIA) to capture baseline knowledge on a specific topic for later analytic use. DIRDs are best understood as reference and synthesis products rather than as original research. It is one of 38 DIRDs produced under the Advanced Aerospace Weapon System Applications Program (AAWSAP) between 2009 and 2011. Because AAWSAP s scope permitted a broad range of supporting topics, not every DIRD in the series directly concerns aerospace systems or future threat assessment. The following summary reflects the DIRD s scope and framing at the time of writing and should not be read as implying current validation of the concepts discussed. This DIRD examines advanced nuclear propulsion for crewed deep-space travel and argues that human missions beyond the Moon would require propulsion systems with both very high thrust and very high specific impulse, which the author contends are difficult to achieve with conventional chemical, nuclear-thermal, and nuclear-electric systems. The report focuses on concepts derived from Project Orion, the discontinued General Atomics nuclear pulse propulsion study sponsored first by ARPA and later by the U.S. Air Force between 1958 and 1965, in which a spacecraft would be driven by repeated nuclear explosions. In this case, the DIRD emphasizes small non-fission-triggered fusion explosions using deuterium, magnetic mirrors, and other unconventional ignition concepts intended to avoid the inefficiencies associated with small fission devices. It presents these ideas as a possible pathway to crewed missions across the solar system, while also linking them to broader visions of long-range human expansion into space. The document is exploratory in character and depends on several unproven ignition methods, enabling technologies, and engineering assumptions. Overall, it is a theoretical examination of fusion-based pulse propulsion concepts rather than as a documentary account of a technology nearing practical realization. Redactions have been made to protect the identity of eyewitnesses, the location of government facilities, or potentially sensitive information about military sites not related to UAP. No redactions have been made to any files released under President Trump's directive concerning information about the nature or existence of any encounter reported as a UAP or related phenomena.
Notable / anomalous element
- If simultaneously detonated from outside, a convergent cylindrical shockwave is launched into the argon. (native PDF text, page 22)
- Using the same physical principles as for deuterium fusion rockets will also lead to the realization of clean nuclear energy, justifying the expenditures for these large projects. (native PDF text, page 7)
- Solution in Between Two Extremes With chemical propulsion, manned space flight to the Moon is barely possible and only with massive multistage rockets. (native PDF text, page 16)
- Two conventional Marx banks charge Drawn From Super Marx generator made up of up one coaxial capacitor/transmission line element to 10 magnetical ly insulated coaxial capacitors into chamber MV. with cylindrical deuterium target. (native PDF text, page 28)
Details
- This product is one in a series of advanced t echnology reports produced in FY 2009 under the Defense Intelligence Agency, Defense Warning Office's Advanced Aerospace Weapon System Applications (AAWSA). (native PDF text, page 2)
- Comments or questions pertaining to l this document should be addressed to lAAP Person 1 AAWSA Program Manager, Defense Intell igence Agency, ATTN: CLAR/DWO3, Bldg 6000, Washington, DC 20340-5100. ii UNCLASSIFIED//509 OFFICIAL 11&ili Qtll. (native PDF text, page 2)
- 1 Deuterium, Argon Ion Lasers, and Kev Superexplosives. (native PDF text, page 3)
- 1 Magnetic Insulation and Inductive Charging. (native PDF text, page 3)
- 4 Deuterium as the Preferred Nuclear Rocket Fuel. (native PDF text, page 3)
- 5 Magnetic Entrapment of the Charged Fusion Products and the Stopping of the Proton Beam in Dense Deuterium. (native PDF text, page 3)
- 6 Solution in Between Two Extremes. (native PDF text, page 3)
- Ignition With 107 -Ampere GeV Proton Beam. (native PDF text, page 4)
Tags: War Department, Nevada, AAWSAP, Technical research, Air Force, Moon, Rocket, Weapons