PARABILIS SPACE TECHNOLOGIES, INC.

Federal contract awards won by PARABILIS SPACE TECHNOLOGIES, INC. (UEI WEMFVUG9KFJ9), 2019–2025 — public record from USAspending.

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

8
awards
$151,006,544,043
total value
2
agencies

Agencies buying from PARABILIS SPACE TECHNOLOGIES, INC.

Department of Defense (4)National Aeronautics and Space Administration (4)

What PARABILIS SPACE TECHNOLOGIES, INC. sells

541715 — RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT NANOTECHNOLOGY AND BIOTECHNOLOGY) (7)541713 — RESEARCH AND DEVELOPMENT IN NANOTECHNOLOGY (1)

Awards

THE CONTRACTOR SHALL PROVIDE ALL NECESSARY MATERIALS, LABOR, EQUIPMENT AND FACILITIES INCIDENTAL TO THE PERFORMANCE OF THIS REQUIREMENT IN ACCORDANCE WITH THE TERMS OF THE ORDER.
Department of Defense · $151,000,000,000 · Dec 29, 2025
PHASE II SBIR - ACOUSTIC FLUID MANAGEMENT DEVICE
National Aeronautics and Space Administration · $849,543 · Jun 5, 2025
FY24 SBIR PHASE II - LOW COST HYBRID ROCKET ORBITAL TRANSFER STAGE
National Aeronautics and Space Administration · $849,934 · Jul 3, 2024
ADVANCED, MODULAR, IN-SPACE, GREEN PROPULSION
Department of Defense · $749,641 · Mar 7, 2022
SBIR III-ADVANCED, ECONOMICAL, IN-SPACE HYBRID PROPULSION
Department of Defense · $1,141,505 · Jun 10, 2021
COVID-19 DIB, SMALL BUSINESS INNOVATIVE RESEARCH AWARD PHASE II, HYBRID ROCKET PROPULSION FOR HYPERSONIC MISSILE DEFENSE RESEARCH
Department of Defense · $1,453,770 · Jun 3, 2020
DEVELOPMENT OF A LOW COST, HIGH PERFORMANCE LAUNCH VEHICLE UPPER STAGE THAT USES A NOVEL AFT INJECTION CENTER EXHAUST (ACE) MOTOR CONFIGURATION WITH 90% HYDROGEN PEROXIDE AND HYDROXYL-TERMINATED POLYBUTADIENE (HTPB) FUEL
National Aeronautics and Space Administration · $749,670 · Aug 8, 2019
PARABILIS SPACE TECHNOLOGIES IS PLEASED TO PROPOSE DEVELOPMENT OF A NOVEL ADDITIVELY MANUFACTURED, DYNAMICALLY-ADJUSTABLE, IN-LINE, CAVITATING FLOW-CONTROL AND MEASUREMENT VENTURI FOR USE IN ADVANCED PROPULSION SYSTEM GROUND TESTING. THIS INNOVATIVE CAPABILITY DRAMATICALLY ADDS TO AND EXTENDS THE ADVANTAGES OF USING A CAVITATING VENTURI TO ISOLATE COMBUSTION CHAMBERS OR OTHER DOWNSTREAM PROCESS FLUCTUATIONS FROM UPSTREAM FEED PRESSURE CONDITIONS. THIS DESIGN WILL GREATLY SIMPLIFY PROPULSION TESTING AND REDUCE COSTS FOR CASES WHERE DESIRED LIQUID FLOW CONDITIONS ARE EITHER NOT PRECISELY UNDERSTOOD OR COVER A RANGE OF HIGH-PRECISION FLOW RATES. THE PROPOSED GEOMETRY IS CAPABLE OF SCALING TO BOTH ULTRA-HIGH PRESSURE AND HIGH FLOW RATE APPLICATIONS. THE PRIMARY INNOVATION CONSISTS OF A UNIQUE FLOATING PINTLE DESIGN AND ASSOCIATED STRUCTURAL SUPPORT WITH BUILT-IN PRESSURE TAPS. THESE PRINTED-IN PRESSURE TAPS PROVIDE BOTH A TOTAL PRESSURE MEASUREMENT UPSTREAM OF THE VENTURI CONTRACTION AND A VENTURI THROAT PRESSURE MEASUREMENT, FACILITATING BUILT-IN FLOW RATE MEASUREMENT AND/OR DETERMINATION OF LIQUID/VAPOR TRANSITION.
National Aeronautics and Space Administration · $749,980 · Jun 26, 2019

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