R-2A Activity · President's Budget PB2027

Revolutionary Propulsion Technology Development

FY2027 Request
$33.3M
▲ 12% vs FY2026
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This activity requests $33.3M in FY2027, 40% of project 623066, up 12% on FY2026. The R-2A exhibit describes it across FY2026–FY2027, including what the FY2027 money is planned to buy.

FY2027 Request
$33.3M
▲ 12% vs FY2026
FY2026 Enacted
$29.7M
▲ 60% vs FY2025
FY2025 Actual
$18.6M
Prior year
Planned work

What the FY2027 request buys

Verbatim from the R-2A exhibit for project 623066 of PE 0602203F. This is the budget justification's own description of work that has not happened yet — the one thing no other level of the budget carries.

FY2027 planned work

Continue evaluation and integration of ramburner rotating detonation engine (RDE) technology. Activities include: -Completion of characterization testing of volume-efficient RDE diffuser concepts -Release of preliminary versions of rapid design RDE computational fluid dynamics codes -Design, fabrication, and testing of novel RDE configurations to explore potential performance improvements -Demonstration of mission relevant integrated RDE design in a direct connect test Continue fan tip generator configuration in future platforms. Activities include: -Experimental characterization of 2nd generation fan tip generator Complete studies in reducing the overall time required for engine development and design cycle a more responsive design times. Activities include: -Completing Concept Design & Military Utility Analysis (MUA) of new advanced propulsion concept -Completing assessment of Digital Engineering Level maturity for internal design process -Assessing digital engineering methods identified in the detailed research plan to shorten the conceptual engine design and vehicle integration time. -Delivery and review of rapid MBSE developed conceptual design models and their generated data Commence and complete design study of variable fan and compressor blades for viability assessment in enabling convertible engines. Activities include: -Variable fan and compressor blades design study. Commence compressor testing for high speed weapons development. Activities include: -Compressor testing

FY2026 to FY2027 change

FY 2027 compared to FY 2026 increased by $3.523 million due to the acceleration of technology development for advanced, air-breathing rotating detonation engines in tactical form factors for long-range, responsive, affordable weapons.

Before the request year

FY2026: the year under way

Prior-year accomplishments and current-year plans from the same exhibit. Context for the FY2027 plan, not a series — an activity partitions its project exactly in the request year, but can under-cover it in earlier years.

FY2026 plans — current year

Continue evaluation and integration of ramburners rotating detonation engine (RDE) technology - Fabricate and test RDE with a subsonic inlet diffuser to assess inlet distortion on integrated performance; - Design, fabricate and test RDE instrumented for quantification of the vibrational environment; - Demonstrate of staged fuel/air RDE injector at scale and relevant conditions; and - Design, fabricate and test of actuated nozzle assembly coupled to scale RDE operated in a water-cooled thermal management arrangement. Continue studies in reducing the overall time required for engine development and design cycle a more responsive design times - Review relevant digital engineering methods identified in the detailed research plan - Conceptual design modifications to commercial off the shelf engines for military application. Complete evaluation of advanced augmentors. Complete studies for exploration of advanced propulsion technologies. - Studies enable initial cycle study on convertible engine. Complete studies in hypersonic combined cycles. Complete analysis of Air Breathing Propulsion Technologies. - Operational benefits and military utility Commence fan tip generator configuration in future platforms. - Experimental characterization of disruptive propulsion. Commence and complete Detailed Design Review of external bearing turbine engines for disruptive propulsion for future platforms. Commence and complete rig testing to advance development of flight ready high-speed engine components.

Money

Three years, and no five-year plan

An R-2A activity publishes the prior year, the current year and the budget year. The FYDP outyears exist at project and program-element level and are deliberately absent here rather than inferred. Estimate types are colored and never summed into one figure.

25018.6FY25ACTUAL29.7FY26ENACTED33.3FY27REQUEST
Actual Enacted Request
Fiscal YearEstimate TypeAmount ($M)
FY2025Actual18.6
FY2026Enacted29.7
FY2027Request33.3

This activity is 40% of project 623066's FY2027 request and 8.4% of PE 0602203F's. In the request year the activities under a project sum to it exactly; in the current year they under-cover it in about 9% of cases, so an activity's delta can legitimately exceed its parent's and the two must not be compared row to row.

Where this sits

10 activities in project 623066

Every R-2A line of this project, largest FY2027 request first. Linked where the activity has enough of its own narrative to carry a page; the rest are shown in full on the project page.

Mission Optimized Air Breathing Propulsion Technology Development$41.5M flat
Revolutionary Propulsion Technology Development — this activity$33.3M ▲ 12%
Aerospace Fuel Technology Development$8.5M NEW
Turbine Engine Components$0.0M
Turboshaft/Turboprop and Turbofan Engine Technologies$0.0M
Engine Technologies for Autonomous Vehicles and Munitions$0.0M
Combustion Technologies$0.0M
Diagnostic Technologies$0.0M
Bearing Technologies$0.0M
Lubricant Technologies$0.0M
Source
FY2027 Department of the Air Force RDT&E Budget Justification · Exhibit R-2A · PE 0602203F, project 623066 (President's Budget PB2027). Congressional marks are recorded on the program element, never on an activity.
Machine access
Markdown twin /programs/0602203F/623066/a1.md · MCP mcp.hitchintel.combudget_get_activity