This solicitation closed on August 19, 2026
View current Department of Defense opportunities →Novel Ignition Systems for multi-pulse Solid Propellant Rocket Motors
AI Overview
This RFP seeks innovative ignition systems for multi-pulse solid propellant rocket motors that can ignite multiple times using the same hardware. The technology aims to reduce reliance on pyrotechnic initiators, lowering inadvertent ignition risks while enabling more flexible propellant utilization and system design.
This summary is AI-generated from the official solicitation.
Key Details
Official Description
Solid propellant propulsion systems which utilize multiple pulses commonly use separate pyrotechnic or pyrogen igniters for each pulse. In recent years, alternative ignition methods have been conceptualized which could ignite rocket motors multiple times with the same ignition hardware. Alternative ignition methods may also eliminate the need for sensitive pyrotechnic initiators typically used in conventional igniters, reducing the danger of inadvertent initiation. Ignition systems which are cap...
Change History
Novel Ignition Systems for multi-pulse Solid Propellant Rocket Motors
Status changed from Open to Closed after topic disappearance
Novel Ignition Systems for multi-pulse Solid Propellant Rocket Motors
**Summary of Changes:** Q1 answer updated: Previously acknowledged as "working to resolve," now directs applicant to contact DoD SBIR Support (DoDSBIRSupport@reisystems.com) for DSIP system technical issues rather than MDA support.
Novel Ignition Systems for multi-pulse Solid Propellant Rocket Motors
This Q&A section documents a resolved technical issue with proposal package creation requiring a title field, and expresses appreciation for the opportunity—neither adds substantive eligibility, requirements, or scope information for prospective applicants.
Novel Ignition Systems for multi-pulse Solid Propellant Rocket Motors
Status changed from Pre-Release to Open
Novel Ignition Systems for multi-pulse Solid Propellant Rocket Motors
New opportunity: Novel Ignition Systems for multi-pulse Solid Propellant Rocket Motors
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