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Digital System-Level Mission-Driven Integrated Design Methods for Aerospace Systems

ID: RFI-AFRL-RQKP-2025-0002 • Type: Special Notice

Description

The Air Force Research Laboratory, Aerospace Systems Directorate (AFRL/RQ) is seeking information on approaches to effectiveness-based military capability development (EBMCD). EBMCD is the process of finding an optimal integrated system
(or system-of-systems) solution that best accomplishes an engagement, mission effect, or campaign goal. It merges two concepts, operational analysis (OA) and system-level physics-based multidisciplinary analysis and design optimization (MDAO). Specific
interest is EBMCD for integrated OA at the mission level along with airframe, propulsion, and power & thermal management systems. Multi-fidelity (low, medium, high) physics based analysis and coupling for the design of integrated airframe, propulsion, and power & thermal management system disciplines is a key underlying attribute supporting the EBMCD vision. Additional attributes of this activity are an emphasis on integrating military utility analysis at the mission level richly within a system design process, increasing the number of system disciplines captured simultaneously in design, and significantly elevating the coupled physics fidelity captured across system disciplines. An ability to rapidly iterate on requirements with mission-driven system-level designs is of interest and is anticipated to engage a wide range of digital engineering and technical disciplines.

Background
The Air Force Research Laboratory, Aerospace Systems Directorate (AFRL/RQ) is focused on enhancing military capability development through effectiveness-based military capability development (EBMCD). This initiative aims to find optimal integrated system solutions that achieve mission effects or campaign goals by merging operational analysis with multidisciplinary design optimization.

The emphasis is on integrated operational analysis at the mission level, particularly concerning airframe, propulsion, and power & thermal management systems. The goal is to improve the design process by integrating various disciplines and increasing the fidelity of physics-based analyses.

Work Details
The contract involves developing a mission-driven system-level design process for aerospace systems, specifically targeting airframe, propulsion, and power & thermal management disciplines. Key tasks include:
- Creating a design process anchored by military utility analysis and measures of effectiveness.
- Ensuring concurrent integration of airframe, propulsion, and power & thermal management disciplines within a multi-fidelity design framework.
- Enabling rapid iteration of requirements with mission-driven designs.
- Reducing late-stage defects due to unmodeled physics.
- Informing technology investment decisions through military utility analysis.
- Ensuring applicability across various air vehicle systems and Mach regimes.

Additionally, the methodology should facilitate improved communication and integration among diverse stakeholders beyond traditional design communities.

Overview

Response Deadline
Dec. 6, 2024, 5:00 p.m. EST Past Due
Posted
Oct. 29, 2024, 6:26 p.m. EDT
Set Aside
None
Place of Performance
Wright Patterson AFB, OH 45433 United States
Source
SAM

Current SBA Size Standard
1000 Employees
Pricing
Multiple Types Common
On 10/29/24 Department of the Air Force issued Special Notice RFI-AFRL-RQKP-2025-0002 for Digital System-Level Mission-Driven Integrated Design Methods for Aerospace Systems due 12/6/24.
Primary Contact
Name
Peter Seiley   Profile
Phone
None

Documents

Posted documents for Special Notice RFI-AFRL-RQKP-2025-0002

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Additional Details

Source Agency Hierarchy
DEPT OF DEFENSE > DEPT OF THE AIR FORCE > AFMC > AIR FORCE RESEARCH LABORATORY > FA2391 USAF AFMC AFRL PZL AFRL RQKP
FPDS Organization Code
5700-FA2391
Source Organization Code
500177445
Last Updated
Dec. 21, 2024
Last Updated By
peter.seiley@us.af.mil
Archive Date
Dec. 21, 2024