TERVES, LLC

Federal contract awards won by TERVES, LLC (UEI NJGYMQDJBBD7), 2019–2025 — public record from USAspending.

Showing awards with a value or ceiling of $250K+ active within the last 5 years. Need older history or smaller awards? Tell us what you need — we expand by request.

awards

expiring in 12 months

agencies

Category award history

4 category awards to a new vendor (same agency and NAICS code, not this contract's own history) — latest: ENGENIUSMICRO LLC took Department of Defense 541715 work from TERVES, LLC (Sep 9, 2025).

Agencies buying from TERVES, LLC

Department of Defense (3)National Aeronautics and Space Administration (1)

What TERVES, LLC has provided

541330 — ENGINEERING SERVICES (1)541713 — RESEARCH AND DEVELOPMENT IN NANOTECHNOLOGY (1)541715 — RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT NANOTECHNOLOGY AND BIOTECHNOLOGY) (1)561790 — OTHER SERVICES TO BUILDINGS AND DWELLINGS (1)

Awards

SMALL BUSINESS INNOVATIVE RESEARCH (SBIR) PHASE II PROPOSAL #L2S-0080 TENDERED UNDER TOPIC #DLA212-004 TO TERVES LLC FOR DOMESTIC PRODUCTION FOR SM AND GD METALS

Department of Defense · $1,491,485 · Dec 18, 2025

TERVES SBIR II PROPOSAL L2-0359 ENTITLED "LOW COST DOMESTIC GADOLINIUM PRODUCTION FOR DEFENSE CRITICAL APPLICATIONS"

Department of Defense · $1,355,690 · Jul 6, 2022

SBIR PHASE II YEAR 2 TOPIC A18-031

Department of Defense · $1,095,461 · Feb 21, 2020

THIS STTR PROGRAM WILL MATURE HIGH DENSITY, HIGH REGRESSION RATE HYBRID ROCKET MOTOR TECHNOLOGY THROUGH TRL6 THROUGH THE DESIGN, FABRICATION, AND TESTING OF THIRD AND FOURTH STAGE NANOSATELLITE MOTORS, WHILE PREPARING DESIGNS AND SIZING FOR BOOSTER STAGES. HYBRID ROCKETS OFFER SUBSTANTIALLY LOWER COST COMPARED TO STORABLE AND CRYOGENIC BIPROPELLANT SYSTEMS, BUT CURRENTLY SUFFER FROM POOR PACKAGING EFFICIENCY. DURING PROOF OF CONCEPT WORK, THE USE OF A HIGH DENSITY, HAN BASED OXIDIZER SYSTEM COMBINED WITH A HIGH DENSITY AND HIGH REGRESSION RATE SOLID FUEL WERE DEMONSTRATED AS SOLUTIONS TO PACKAGING EFFICIENCY, O/F RATIO SENSITIVITY, AND REGRESSION RATE LIMITATIONS OF HYBRID MOTORS. THE HAN BASED OXIDIZER HAS LOW FREEZING TEMPERATURE AND NO APPRECIABLE VAPOR PRESSURE, BEING SAFE, STORABLE, AND ELIMINATING THE NEED FOR SPECIAL HANDLING AND SHIPPING PRECAUTIONS. THE HIGH DENSITY OXIDIZER COMBINED WITH THE HIGH DENSITY, HIGH PERFORMANCE FUEL, CREATES A HYBRID ENGINE SYSTEM WITH THE DENSITY IMPULSE PERFORMANCE OF A SOLID ROCKET MOTOR, BUT THE THROTTLEABILITY OF A BIPROPELLANT SYSTEM, WITH THE SAFETY APPROACHING AN INERT SYSTEM. AN ELECTRICALLY ENHANCED IGNITION SYSTEM WAS DEMONSTRATED WHICH IMPROVED C*, AND ENABLES HIGHER PERFORMANCE TO BE MET WITH SHORTER MOTOR GRAINS, WITH THE POTENTIAL FOR MULTIPLE START CAPABILITIES. THIS PHASE II PROGRAM WILL CONTINUE THE DEVELOPMENT OF HIGH DENSITY, SAFE, STORABLE, NON-TOXIC HYBRID MOTORS TO OPTIMIZE ISP AND MOTOR DESIGN, IMPROVE INJECTOR AND IGNITER PERFORMANCE, AND MATURE THIRD AND FOURTH STAGE MOTOR MATURITY THROUGH FULL SCALE MOTOR BURNS.

National Aeronautics and Space Administration · $747,824 · Apr 16, 2019