ACENT LABORATORIES LLC

Aerospace · Private

Mid-air recovery systems and deceleration mechanisms for hypersonic flight test vehicles and components

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Updated · acentlabs.com

Sector
Aerospace
Total capital
$12.7M
Federal grants
$2.5M
2 awards · 2015–2017
Rank in peer group#79 of 89
Private capital raised
None on recordNo Form D filings on SEC EDGAR. Some raises are not filed.
Federal contracts
$10.2M
13 awards · NASA, Defense
Rank in Aerospace#229 of 1335
Granted patents
0
1 pending

Capital timeline

201020122014201620182020FEDERAL ↑EQUITY ↓Cumulative $12.7M$1.9M$750K$4.1M$1.2M$1.7M$750K
201020122014201620182020FEDERAL ↑EQUITY ↓Cumulative $12.7M$1.9M$4.1M$1.7M

Latest events

  • Federal contractDefense · Enabling Technologies For High Speed Operable (ethos), Economical Test Facility Fuel Heater$298K
  • Federal grantDefense · Phase II · Recovery Method for Unmanned Hypersonic Test Vehicles$750K
  • Federal contractNASA · Igf::ot::igfnasa Has Identified Nuclear Thermal Propulsion (ntp) As A Concept Than Can Provide The Fastest Trip Times To Mars And As The Preferred Propulsion Concept For Human Space Travel. The Current NASA Strategic Space Technology Investment Plan States Ntp Is A High Priority Technology Needed For Future Human Exploration Of Mars. The Ntp Concept Is Similar To A Liquid Chemical Propulsion System, Except In Lieu Of Combustion In The Thrust Chamber, A Fission Reactor (heat Exchanger) Heats A Mo$250K
  • Federal contractDefense · Igf::ot::igf Recovery Method For Unmanned Hypersonic Test Vehicle$150K
  • Federal grantNASA · Phase II · Hydrogen Wave Heater for Nuclear Thermal Propulsion Component Testing$1.7M
  • Federal contractNASA · Igf::ot::igf NASA Has Identified Nuclear Thermal Propulsion (ntp) As An Approach That Can Provide The Fastest Trip Times To Mars And As The Preferred Concept For Human Space Travel. In Order To Perform Component Testing In Support Of Ntp Engine Development, An Efficient Means For Delivering High-flow Rate, High Temperature, Hydrogen Is Required. Non-nuclear Generation Of The Desired Hydrogen Flow Rates And Temperatures For Ground Test Of Ntp Components And Subsystems Is Problematic. Acent Labora$1.2M
  • Federal contractNASA · Igf::ot::igf NASA Has Identified Nuclear Thermal Propulsion (ntp) As A Propulsion Concept Which Could Provide The Fastest Trip Times To Mars And As The Preferred Concept For Human Space Travel. The Current NASA Strategic Space Technology Investment Plan States Ntp Is A High Priority Technology Needed For Future Human Exploration Of Mars. In Order To Perform Component Testing In Support Of Ntp Engine Development, An Efficient Means For Delivering High-flowrate, High-temperature Hydrogen Is Requir$124K
Show 8 earlier federal awards
  • Federal contractDefense · Igf::ot::igf Enhanced Operability Of Scramjet Tech, Systems Engineering&design Support For Cold Starttechnologies$4.1M
  • Federal contractDefense · Igf::ot::igf Low Cost Modular Approach To Flight Testing Of Hypersonic Systems$750K
  • Federal contractDefense · Igf::ot::igf - Mscc Instrumentation Section$148K
  • Federal contractDefense · Igf::ot::igf Medium Scale Scramjet Fuel System Development$1.9M
  • Federal contractDefense · Distortion Generator Development$367K
  • Federal contractDefense · Low Cost Hyper Systems Flight Testing - Acent Lab$149K
  • Federal contractNASA · This Proposal Leverages A Highly Successful Phase 1 Feasibility Effort To Further Develop A System That Satisfies The Cold-start Requirements Of Scramjet Engines. The System Provides Energy-dense, Low Volume Hydrocarbon Fuel Conditioning Based On The Hydrolysis Reaction Of Triethylaluminum (tea) With Water. Tea Is An Organometallic Liquid That Reacts Exothermically With Water And Burns Readily In Air. In Phase 1, We Demonstrated The Hydrolysis Of Tea In Jp Fuel Within An Integrated Mixing/inject$599K
  • Federal contractNASA · This Proposal Addresses The Cold-start Requirements Of Scramjet Engines By Developing A Safe, Energy-dense, And Low Volume Hydrocarbon Fuel Conditioning System Based On The Hydrolysis Reaction Of Water With Triethylaluminum (tea). Tea Is An Organometallic Liquid That Reacts Exothermically With Water And Burns Readily In Air When Not Diluted In Hydrocarbon Mixtures. We Propose To Use The Hydrolysis Of Nonpyrophoric Dilute Tea/jp Fuel Mixtures In An Integrated Mixing/injection Apparatus To Heat An$99K

Node area is scaled to amount. Form D reports securities sold, which can differ from an announced round; filings are numbered in the order they were made.

Standing among 89 peers

Line = median

Aerospace · System

  • Federal grantsBelow median

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Founders and team

No founders are linked to this company yet.

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Checked: USPTO inventors; federal award principal investigators; SEC Form D related persons · Oct 23, 2026

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What it has protected

USPTO · 0 granted of 1
  • PendingInertial Extraction SystemUSPTOApplication PCTUS2012053180

Regulatory activity · Aerospace

Sector-level, not company-level

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Sources

Federal grants from SBIR/STTR, NIH, NSF and DoD records. Federal contracts from USAspending.gov. Private capital from SEC Form D. Patents from USPTO. Publications from OpenAlex. Regulatory activity from the Federal Register. Press matched on company name.

How to read this page

Figures show associations in public records, not causes or predictions. Nothing here is investment advice. An em-dash means no record was found under this company's name, not that none exists.

Data freshness

SEC Form D filings through . SBIR and STTR awards through .