Scalable Agile Manufacturing of Launched Effects

Opportunity ARM26BX02-NV004 no longer available

**Summary of Q&A Changes:** One new Q&A was added (Q1) explicitly clarifying that the initiative focuses exclusively on structural airframe manufacturing and excludes all electronics. This represents a significant clarification that was not previously addressed. All other Q&As (Q2-Q8) remain substantively identical to the previous version, with only minor renumbering due to the new Q1 insertion. No previously pending responses were resolved, and no technical requirements, eligibility criteria, or budget/timeline information were updated.

**Key Changes to Q&A:** 1. **NEW Q1** – Clarifies the $2,000 airframe cost target excludes payload costs; payload is separate. 2. **Previous Q1-Q7 renumbered to Q2-Q8** – All prior answers remain substantively unchanged but reordered. **Summary:** One new clarification added on cost scope (payload excluded from $2,000 target). No substantive changes to existing guidance on design vs. process focus, aspirational targets, material flexibility, tube-launch requirements, or Phase I budget ($300,000).

Status changed from Pre-Release to Open

# Q&A Changes Summary **One new question added (Q1):** Clarifies that the topic accepts either design-for-manufacturing OR manufacturing process solutions; evaluation will assess the entire approach's reasonableness; and tube-launch capability is important but preliminary designs don't need complete fielding engineering. **All previously answered questions retained** with identical responses. No answers were updated or clarified further.

# Q&A Changes Summary **New Q&A added (Q1):** Four clarifications on key evaluation criteria: - Cost ($2K) and rate (10K/month) targets are **aspirational, not hard thresholds** for Phase I - Design-change reconfiguration can be achieved via software or physical tooling changes - No prescribed structural performance floor; evaluation based on improvement over state-of-the-art - Phase I emphasis on demonstrating Phase II feasibility; relative weight of process maturity vs. modeled approach depends on technology maturity and complexity **Previous Q&As (Q2-Q6):** Renumbered without substantive changes.

Added new Q2 clarifying airframe scope (structural features only, no non-structural systems design required), tube geometry (offeror-defined), and design-change adaptability evaluation criteria. Renumbered subsequent Q&As accordingly.

Added 1 new Q&A clarifying material and manufacturing flexibility: thermoset composites allowed, no material type restrictions, and partnership with qualified LE-SR vehicle not required. Existing Q&As (design specs, $300K Phase I limit, tube-launch requirement) renumbered but unchanged.

Added 1 new Q&A (Q3) clarifying that the aircraft must be designed specifically for tube-launch, with manufacturing considerations across the entire vehicle structure.

Added 1 new Q&A (Q1) providing technical guidance on feasibility study design parameters: clarifies that performance metrics should be appropriate to airframe size rather than prescriptive dimensions/weights, identifies major load cases (launch, aerodynamic, handling), and notes no public reference designs available. Previous typo correction (Phase I $300K limit) moved to Q2.

This Q&A clarifies that Phase I submissions have a maximum cost limit of $300,000 (not $3,000,000 as stated in the original document due to a typo) with a performance period of 1-6 months.

New opportunity: Scalable Agile Manufacturing of Launched Effects