Documents / Official release
This Defense Intelligence Reference Document (DIA-08-1011-001), dated 1 November 2010, was prepared by the Defense Intelligence Agency's Defense Warning Office under the Advanced Aerospace Weapon System Applications program. It covers nanosatellite technologies, laser Lightcraft propulsion, a weapon mission selection study and a multi-megawatt laser study. The author recommends that the Department of Defense, working with NASA, bring laser Lightcraft propulsion research back to the United States and restart the Air Force X-50LR test flight program.
From the source:Release of 2026-09-18 Incident: 11/1/10, Las Vegas, Nevada. Released with redactions. 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 laser-propelled “Lightcraft” as a possible low-cost method to launch very small satellites into low Earth orbit by using a remote high-energy laser to supply most of the propulsion energy rather than relying entirely on onboard energy sources. The report combines a survey of nanosatellite trends with a review of “Lightcraft” propulsion concepts, vehicle design, beam-control requirements, and mission studies, and argues that the most promising application is the launch of nano- or pico-satellites, especially Earth- and space-observing payloads of a few kilograms or less. It presents the concept as potentially much cheaper than conventional multistage rockets for very small payloads, while also noting significant practical constraints including strict beam-riding geometry, atmospheric losses, demanding pointing and adaptive-optics requirements, and heavy dependence on large ground-, sea-, or air-based laser infrastructure. Overall, the document presents laser “Lightcraft” as a technically plausible launch concept whose attractiveness depends on whether the supporting laser and beam-control system can be made reliable and economical at operational scale.
“Sea”14 pages
UNCLASSIFIED/;'POR: OPPICIAL USE 014Lf system, like the air-to-air one, has reduced capability if an enemy ca n achieve nea rly simultaneous arriva l times for all of its ballistic missiles. If so, then a Lig htcraft BMD system would have to serve as an adjunct to ot her BMD systems, such as the ground based PAC-3 Patriot, THAADS, or NMD which are deployed for nat ional or theater ballist ic missile defense. However, this system could protect regions agai nst limited ballistic missi le attacks at the earliest phase of hostilities before ground-based BMD systems cou ld arrive and be deployed. Table 4. Influence of Target Velocity and Intercept Angle on Impact Energy and Required Mass [261. Lightcraft Intercept Velocity Lightcraft Intercept Aspect Impact Energy and Weight Ballistic Missile Threat -SRBM--IRBM--ICBM- R~l000 km R~2500km R~l0,000 km V=l km/s V=4 km/s V=6km/s 0° from Impact E for 1.0 kg Wt. 25MJ 49MJ 81 MJ Bead-on Collision Wt for 10 MJofE .40kg .20 kg .12 kg 30° from Impact E for 1.0 kg Wt. 21 MJ 44MJ 74MJ 3 km/s Bead-on Collision Wt. For 10 MJofE .47 kg .23 kg .14 kg 45° from Bead-on Collision Impact E for 1.0 kg Wt. 17MJ 37MJ 66MJ Wt. for 10 MJofE .59 kg .27kg .15 kg UNCLASSIFIED,'fFOA QFFISIAL 1!181!! 8HLY 34
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Official release, from the pursue collection. The PDF is mirrored here; the original link is under it. 77 pages are in the text index: search them above, or from the library's search.