Exquadrum: Prime Awards
All 80 federal prime contract awards since FY2008, $66.1M obligated, including subsidiaries. Largest obligation first.
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Awards 1–80 of 80 · page 1 of 1
- Operational Fires (Opfires) Propulsion System. the Opfires Propulsion System Task Will Be A Two-phased Effort to Design and Develop Innovative Propulsion Concepts and Technologies Enabling A Novel Ground-launched System for Tactical Weapons Deployment. · Defense Advanced Research Projects Agency · USAspending ↗$13.1M
- Laredo · U.S. Air Force · USAspending ↗$6.5M
- Management Administrative Services · U.S. Air Force · USAspending ↗$3.2M
- Ultra-vk Exoatmospheric Flight Test · Missile Defense Agency · MDA SUPPORT · USAspending ↗$3.0M
- Sbir Phase II Research and Development · Missile Defense Agency · MDA SUPPORT · USAspending ↗$2.6M
- IGF::OT::IGF Nra Advanced Development Affordable Upper Stage Engine Systems Requirements Study for the Space Launch System Advanced Development Office. the System Requirements Study Consists of Four Major Sub-tasks: Trade Studies and Requirements Analysis, Recurring / Nonrecurring Costs and Schedule, Modular Aerospike Rocket Engine, and Documentation · NASA · USAspending ↗$2.5M
- Logistics and Munitions Services · U.S. Air Force · USAspending ↗$2.3M
- Sbir/sttr Phase II R&D Ultra Interceptor Stage · Missile Defense Agency · MDA SUPPORT · USAspending ↗$2.3M
- Sbir Direct to Phase II: Low Cost Objective Kinetic Interceptor Dacs (Loki Dacs) · Missile Defense Agency · MDA SUPPORT · USAspending ↗$2.0M
- IGF::OT::IGF Consolidated Hazardous&energetic Material Management Services (Chemms) · U.S. Air Force · USAspending ↗$2.0M
- Sbir III - Kinetic Fireball Payload · Defense Threat Reduction Agency · USAspending ↗$1.9M
- IGF::OT::IGF DARPA Sbir Phase II · U.S. Army · USAspending ↗$1.5M
- IGF::OT::IGF Phase II Sttp Novel Upper Stage Engine Cycle Phase II · U.S. Air Force · USAspending ↗$1.5M
- Sbir/sttr Phase II R&D Dacs Verde Ph II · Missile Defense Agency · MDA SUPPORT · USAspending ↗$1.5M
- Sbir/sttr Phase II R&D: Insensitive for Tactical Applications (Iota) · Missile Defense Agency · MDA SUPPORT · USAspending ↗$1.5M
- IGF::OT::IGF Sbir Phase II Solid Liquid Intergrated Cycle Engine (Slice) · U.S. Air Force · USAspending ↗$1.5M
- Sbir Ph II Topic&prototype Ussocom 17.1 Topic 003 · U.S. Special Operations Command · USAspending ↗$1.3M
- IGF::OT::IGF Sttp 2012-09 · U.S. Air Force · USAspending ↗$1.1M
- IGF::OT::IGF Sbir Phase II Research&dev · Missile Defense Agency · MDA SUPPORT · USAspending ↗$1.1M
- Sbir/sttr Phase II R&D - Neptune Green Propellant Target Stage · Missile Defense Agency · MDA SUPPORT · USAspending ↗$1.0M
- Sbir Phase II, Cost Plus Fixed Fee Type Contract. the Objective of the Proposed Advanced Research for Controllable, Highly Efficient Rocket Propulsion (Archer) Phase II Is to Develop and Deminstrate and Innovative, High-performing Solid Propellant That Would Enable A Lightweight Dacs with A High Mass Fraction That Would Be Agile Enough to Provide A Very Small, Minimum Propulsive Impulse Bit. This System Would Also Be Highly Efficient, Environmentally Friendly, and Show Good Promise of Meeting Insensitive Munitions Requirements. the Propellant Being Developed Would Meet US Navy Requirements for A Solid Propellant Dacs on Navy Vessels. · U.S. Army · USAspending ↗$984K
- High Temperature Incendiary Device Design, Test and Study. · U.S. Army · USAspending ↗$955K
- During the Proposed Phase II Research and Development Effort, the Project Team Will Complete the Integration of Previously Demonstrated Technologies Into An Upper Stage Propulsion System for A Small Launch Vehicle (Slv). the Resulting Stage Will Meet Launch Vehicle Requirements for Mass Fraction and Specific Impulse. the Phase II Project Will Result in the Hot-fire Qualification of A Flight-weight Upper Stage in A Static Test. the Proposed Project Team Will Develop A Plan for A Potential Follow-on Phase II Flight Demonstration Program. · NASA · USAspending ↗$750K
- Sbir Phase II, Proposal T2-0166 · Defense Threat Reduction Agency · USAspending ↗$742K
- IGF::OT::IGF Sbir Phase II - Novel Upper Stage Engine Cycle · U.S. Air Force · USAspending ↗$739K
- Sbir II - Exquadrum · U.S. Air Force · USAspending ↗$738K
- Army Sbir Phase II · U.S. Army · USAspending ↗$730K
- IGF::OT::IGF the Objective of the Proposed Research and Development Effort Is to Demonstrate the Feasibility of An Innovative Approach to High-performance Hybrid Propulsion for Upper-stages. the Missions for These Propulsion Systems Include Launching Small- and Nano-satellites and Conducting Hypersonic Flight Test Operations. the Focus of the Research Effort Will Be on Achieving High Specific Impulse by Means of An Innovative Approach to Nozzle Design. the Technology Will Be Experimentally Demonstrated in A Series of Hot-fire Tests During the Proposed Research Program. · NASA · USAspending ↗$700K
- Supplies · U.S. Special Operations Command · USAspending ↗$499K
- AF04-287 · U.S. Air Force · USAspending ↗$344K
- 200612!000435!5700!FA9101!AEDC/PKP !FA910106C0119 !A!n! !N! ! !20060929!20081001!126112387!126112387!126112387!N!EXQUADRUM, Inc !12130 Rancho Rd !Adelanto !CA!92301!00296!071!06!ADELANTO !San Bernardino !CALIFORNIA!+000000300000!N!N!000000649978!AD95!RDTE/OTHER Defense-eng/manuf Develop !S1 !Services !000 !Not Discernable !541710!E! !3! ! ! ! ! !99990909!B!F!N!A! !A!N!U!2!009!K! !Z!y!z! ! !N!b!n!n! ! !Z! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! · U.S. Air Force · USAspending ↗$225K
- Develop An Innovative Materiel Solution Utilizing Phase Change Materials Tailored for Thermal Regulation Within A Closed-circuit Self-contained Breathing Apparatus to Reduce Thermal Burden. · U.S. Army · USAspending ↗$210K
- Kinetic Fireball Incendiaries - Sbir III · Defense Threat Reduction Agency · USAspending ↗$198K
- E014042 Sbir Phase I Small Spacecraft Transfer-stage Aluminized Rocket (Small Star) · NASA · USAspending ↗$156K
- E014042 Sbir Phase I Extraterrestrial Sample-return Chemistry for Advanced Propulsion Experiment (Escape) · NASA · USAspending ↗$156K
- FY24 Sbir Phase I- Zebra Aerospace Engine · NASA · USAspending ↗$156K
- Sbir/sttr Phase I Research & Development · Missile Defense Agency · MDA SUPPORT · USAspending ↗$155K
- Sbir/sttr Phase I Research & Development · Missile Defense Agency · MDA SUPPORT · USAspending ↗$155K
- Sbir Phase I Research & Development, Ultra Interceptor Stage · Missile Defense Agency · MDA SUPPORT · USAspending ↗$155K
- IGF::OT::IGF the Purpose of This Procurement Is for the Purchase of Modification to A 70 Lb. Peacekeeper Attitude Control Engine (Ace) Engine for Operation with Commercially Available Liquid Ethylene Nitrous Oxide (Leno) "Green" Propellant and Hot Fire the Engine. · NASA · USAspending ↗$150K
- IGF::OT::IGF Feasibility Study, Sbir Phase I, Topic SOCOM171- 003, Innovative Cubesat Payloads for Ussocom Space Missions · U.S. Special Operations Command · USAspending ↗$150K
- Sbir I, "Novel Upper Stage Engine Cycle" · U.S. Air Force · USAspending ↗$150K
- IGF::OT::IGF Multi-mode On-board Power Generation · U.S. Air Force · USAspending ↗$150K
- Ph I Research&development-powder Rocket with Improved Mass-fraction and Agility (Prima) IGF::OT::IGF · Missile Defense Agency · MDA SUPPORT · USAspending ↗$150K
- IGF::OT::IGF Sbir/sttr Phase I Research&development,proposal Number: B172-010-0100, Proposal Title: Novel Energetic Propellant Technology for Ultimate Netcentric Efficiency (Neptune) · Missile Defense Agency · MDA SUPPORT · USAspending ↗$150K
- Sbir Phase I - FA93000-12-M-1005 · U.S. Air Force · USAspending ↗$150K
- Performance of Work in Accordance with · U.S. Army · USAspending ↗$150K
- IGF::OT::IGF - Base Period - Sbir Phase I - Entitled "Low-cost Turbopump for Expendable Launch Technology" Dated 6/23/2015. · U.S. Army · USAspending ↗$150K
- Sbir Phase 1 Contract Award · U.S. Navy · USAspending ↗$146K
- During the Proposed Phase I Research and Development Effort, the Project Team Will Integrate Previously Demonstrated Technologies Into A Low-cost Solid Rocket Motor to Serve As A Cis-lunar Transfer Stage to Guide and Propel Small Spacecraft on Trans · NASA · USAspending ↗$131K
- IGF::OT::IGF Exquadrum Proposes A High-performance Liquid Bi-propellant Rocket Engine That Uses Propellants That Are Non-toxic, Self-pressurizing, and Low Cost. the Proposed Engine and Propellants Provide the Same Performance As State-of-the-art Storable Propellants. the Propellants Are Storable for Long Durations Without Decomposition or Degradation. Because the Propellants Are Self-pressurizing, They Offer the Potential for Overall System Weight Savings by Eliminating the Pressurization System. in Phase I, Exquadrum Will Develop This Engine Concept Through Trade Studies and Analyses and Conclude with A Proof-of-concept Hot Fire Demonstration of A Full-scale Laboratory Engine. in Phase II, Exquadrum Ill Mature the Engine Design to Detail Design, and Deliver A Full-scale Laboratory Engine. in Phase II, Exquadrum Will Mature the Engine Design to Detail Design, and Deliver A Full-scale Engine to NASA for Functional and Environmental Testing Under Simulated Mission Conditions. · NASA · USAspending ↗$125K
- The Objective of the Proposed Research and Development Effort Is to Demonstrate the Feasibility of An Innovative Approach to High-performance Hybrid Propulsion for Upper-stages. the Missions for These Propulsion Systems Include Launching Small- and Nano-satellites and Conducting Hypersonic Flight Test Operations. the Focus of the Research Effort Will Be on Achieving High Specific Impulse by Means of An Innovative Approach to Nozzle Design. the Technology Will Be Experimentally Demonstrated in A Series of Hot-fire Tests During the Proposed Research Program. · NASA · USAspending ↗$125K
- Exquadrum Proposes to Develop and Demonstrate A Highly-controllable, Microsatellite Scale Hybrid Orbital Propulsion System (Hops) Utilizing Nitrous Oxide Oxidizer and An Exquadrum Proprietary Solid Fuel Formulation. the Proposed System Is High-thrust, Readily Scales Between Cubesat Sizes From 3U to 27U, and Is Capable of Achieving Impulse Densities Up to 1,300 Ns/u. the Hybrid Thruster Powering the System Is Electrically Ignited and Capable of Numerous Restarts, with the Number of Thrust Pulses Limited Only by the Propellant Supply. During the Proposed Phase I Project, Exquadrum Will Create A Preliminary Design of the Propulsion System and Conduct A Hot-fire Demonstration of A Heavyweight Thruster Prototype. · NASA · USAspending ↗$125K
- IGF::OT::IGF the Objective of the Proposed Research and Development Effort Is to Demonstrate the Feasibility of A Pyrotechnic Igniter System That Is Capable of An Almost Unlimited Number of Reignition Events for Extinguishable Solid Rocket Motors. the Igniter System Will Be Capable of Rapid Motor Ignition Over Range of Conditions From Sea Level to Vacuum. the Technology Will Be Experimentally Demonstrated During the Propose Research Project. · Missile Defense Agency · MDA SUPPORT · USAspending ↗$125K
- Sbir/sttr Phase I Research & Development-solid Propellant Infrared Reduction at Launch (Spiral) · Missile Defense Agency · MDA SUPPORT · USAspending ↗$125K
- Base - Sbir Phase 1 · U.S. Navy · Trident II D5 missile · USAspending ↗$125K
- IGF::OT::IGF During the Proposed Phase I Research and Development Effort, the Project Team Will Integrate Previously Demonstrated Technologies Into A Stage 4 Propulsion System for An Existing Small Launch Vehicle (Slv). the Resulting Fourth Stage Will Meet Launch Vehicle Requirements for Mass Fraction and Specific Impulse. Key Stage Component Will Be Fabricated and Demonstrated. the Propulsion System Will Be Evaluated in A Hot-fire Test Series. the Proposed Project Team Will Develop A Plan for A Potential Follow-on Phase II Flight Demonstration Program. · NASA · USAspending ↗$125K
- Sbir/sttr Phase I Research&development - Equester Green Propellant Turbopump · Missile Defense Agency · MDA SUPPORT · USAspending ↗$100K
- Technical Data · U.S. Special Operations Command · USAspending ↗$100K
- Contract Summary Report. · Missile Defense Agency · MDA SUPPORT · USAspending ↗$100K
- Exquadrum, Inc. Proposes to Demonstrate the Feasibility of An Innovative Approach to Providing NASA with A Guided Dropsonde (Ngd). Nasa's Desire to Use Existing Aircraft Systems Such As the Avaps Aboard Nasa/noaa P-3 Aircraft Will Be Met by Incorporating Existing Dropsonde Sensors with Innovative Aerodynamics, Deployment Structures, and Programmable Control Packages to Facilitate More Accurate Observations in Extreme Conditions. · NASA · USAspending ↗$100K
- Sbir Phase I Osd Topic No. 08-PR3 · U.S. Air Force · USAspending ↗$100K
- Phase I Sbir · U.S. Air Force · USAspending ↗$100K
- Sbir Phase I Osd Topic 08-PR4 · U.S. Air Force · USAspending ↗$100K
- Ph I Research&development · Missile Defense Agency · MDA SUPPORT · USAspending ↗$100K
- Monthly Progress Reports - Sbir Phase I · Defense Threat Reduction Agency · USAspending ↗$100K
- Ph I Research & Development · Missile Defense Agency · MDA SUPPORT · USAspending ↗$100K
- Sbir 18.2 Phase I Research&development for Zero-stage Operationally Range-independent Gantry (Zorg) · Missile Defense Agency · MDA SUPPORT · USAspending ↗$100K
- DARPA Sbir Phase I · U.S. Army · USAspending ↗$99K
- Incendiary Devices · U.S. Army · USAspending ↗$76K
- Base Period: Low Visibility Decoy Flare · U.S. Special Operations Command · USAspending ↗$75K
- Radiation-tolerant Advanced Defense Interceptor Upper Stage (Radius) · U.S. Air Force · USAspending ↗$75K
- Research · U.S. Army · USAspending ↗$70K
- High Temp Incendiary Device · U.S. Army · USAspending ↗$65K
- Additively Manufactured Solid-propulsion for Affordable Mass · U.S. Air Force · USAspending ↗$50K
- Army Sbir Bridgegap · U.S. Army · USAspending ↗$50K
- Scalable Homeland Innovative Enterprise Layered Defense (Shield) Initial Order. · Missile Defense Agency · USAspending ↗$500
- Minimum Guarantee Task Order for Associated Seaport Nxg Mac Awards. · U.S. Navy · USAspending ↗$500
- 200505!000081!5700!FA9300!AFFTC/PKT !FA930005C0009 !A!n! !Y! ! !20050127!20070427!126112387!126112387!126112387!N!EXQUADRUM, Inc !12130 Rancho Rd !Adelanto !CA!92301!00296!071!06!ADELANTO !San Bernardino !CALIFORNIA!+000000746446!N!N!000000746446!AC21!RDTE/MISSILE and Space Systems-basic Research !A2 !Missile and Space Systems !000 !* !541710!E! !3! ! ! ! ! !20200930!B! ! !A! !A!N!U!2!003!K! !Z!y!z! ! !N!b!n!n! ! !Z! !B!A!000!C!B!N! ! ! ! ! ! !0001! ! · U.S. Air Force · USAspending ↗$0
- 200411!000717!5700!GS05 !Det 8 Afrl/pk (Supports Vs) !FA945304C0315 !A!n! !Y! ! !20040812!20061116!126112387!126112387!126112387!N!EXQUADRUM, Inc !12130 Rancho Road !Adelanto !CA!92301!00296!071!06!ADELANTO !San Bernardino !CALIFORNIA!+000000550000!N!N!000000719526!AC11!RDTE/AIRCRAFT-BASIC Research !A2 !Missile and Space Systems !Caa !MDA Support !541710!E! !3! ! ! ! ! !99990909!B! ! !B! !A!N!U!2!002!K! !Z!y!z! ! !N!b!n!n! ! !Z! !B!A!00 !C!b!n! ! ! ! ! ! !0001! ! · Defense Contract Management Agency · MDA SUPPORT · USAspending ↗−$722