FederalOH
Posted
Oct 7, 2026
Oct 19, 2026
Sleeve, Propulsion Shaf - SPE7M427T0395 (Request for Quotation)
Sleeve, propulsion shaf; NSN 2010015104433, Qty 4 UI EA.
Description: The Defense Logistics Agency is requesting quotes for four propulsion shaft sleeves (NSN 2010015104433), for delivery to DLA Distribution within 297 days after order. The solicitation identifies approved source part numbers 96169 H7130105-3 and 96169 H7130105B-3, and requires electronic quotations from responsible sources. It is a total small-business set-aside, and specifications, plans, and drawings are not available.
Federal · VA, US
Original attachments and procurement documents tied to this bid.
Federal RFP files are for Starbridge customers only.
You can request RFP files from all other buyer types for free on this site.
Adjacent opportunities open for bidding right now.
FederalOH
Posted
Oct 7, 2026
Oct 19, 2026
Sleeve, propulsion shaf; NSN 2010015104433, Qty 4 UI EA.
Posted
Sep 23, 2026
Oct 23, 2026
This is a DARPA Small Business Technology Transfer (STTR) Direct-to-Phase-II topic under the DoW 2026 STTR Broad Agency Announcement, focused on space technology. It seeks a fuel-flexible spacecraft electric-propulsion system that can efficiently operate on air, water, or water/carbon-dioxide or nitrogen/hydrogen mixtures at greater than 30% electrical efficiency. Applicants must demonstrate prior performance and durability evidence, while the Phase II effort integrates and qualifies the thruster, power-processing, flow-control, and bus-interface systems for later spaceflight transition.
Special DistrictTX
Posted
Oct 1, 2026
Oct 28, 2026
Rebuild miscellaneous electronic rail propulsion components.
Posted
Mar 24, 2026
Mar 2, 2027
In mono-propulsion systems, a propellant is flowed across a catalyst to promote a chemical reaction and generate thrust. Conventional catalyst manufacturing methods entail (a) coating the inner walls of the thruster nozzle with a catalyst (generally undesirable due to limited catalyst-propellant contact), or (b) inserting a metal or graphite foam coated with a catalyst material into the thruster chamber. Method (b), while superior in terms of thrust generation, also possesses several limitations. Metal/graphite foams are difficult and expensive to procure, stochastic/random in nature (e.g., possess high variability in terms of geometric and other properties), and must be jammed into the thruster chamber using a compression plunger during installation – a process that often leads to catalyst damage. A new manufacturing method that improves repeatability, thruster reactivity, and tailorability (e.g., mechanical, chemical, and fluid flow) while reducing cost and lead time is thus highly desirable. To address this need, NASA and EOS developed methods to additively manufacture (AM) ultra-fine lattice structure propulsion catalysts.
Decision makers connected to this RFP from Defense Logistics Agency.