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  5. CLEAR SCIENCE CORP.

CLEAR SCIENCE CORP.

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Company Details

Name: CLEAR SCIENCE CORP.
Jurisdiction: New York
Legal type: DOMESTIC BUSINESS CORPORATION
Status: Active
Date of registration: 22 Mar 2001 (24 years ago)
Entity Number: 2619331
ZIP code: 13784
County: Cortland
Place of Formation: New York
Address: PO BOX 233, HARFORD, NY, United States, 13784
Principal Address: 663 OWEGO HLL RD, HARFORD, NY, United States, 13784

Shares Details

Shares issued 200

Share Par Value 0

Type NO PAR VALUE

DOS Process Agent

Name Role Address
C/O HENRY A CARLSON DOS Process Agent PO BOX 233, HARFORD, NY, United States, 13784

Chief Executive Officer

Name Role Address
HENRY A CARLSON Chief Executive Officer 663 OWEGO HILL RD, HARFORD, NY, United States, 13784

Unique Entity ID

CAGE Code:
1UY19
UEI Expiration Date:
2020-07-16

Business Information

URL:
www.clearsciencecorp.com
Activation Date:
2019-07-17
Initial Registration Date:
2001-08-18

Commercial and government entity program

CAGE number:
1UY19
Status:
Active
Type:
Non-Manufacturer
CAGE Update Date:
2024-03-09
CAGE Expiration:
2027-03-08
SAM Expiration:
2023-04-05

Contact Information

POC:
HENRY A. . CARLSON
Corporate URL:
www.clearsciencecorp.com

Form 5500 Series

Employer Identification Number (EIN):
161603092
Plan Year:
2019
Number Of Participants:
2
Sponsors Telephone Number:
6078449171
File:
View File
Plan Year:
2019
Number Of Participants:
2
Sponsors Telephone Number:
6078449171
File:
View File
Plan Year:
2018
Number Of Participants:
2
Sponsors Telephone Number:
6078449171
File:
View File
Plan Year:
2017
Number Of Participants:
2
Sponsors Telephone Number:
6078449171
File:
View File
Plan Year:
2016
Number Of Participants:
2
Sponsors Telephone Number:
6078449171
File:
View File

History

Start date End date Type Value
2001-03-22 2003-03-05 Address PO BOX 233, HARFORD, NY, 13784, USA (Type of address: Service of Process)

Filings

Filing Number Date Filed Type Effective Date
130404002045 2013-04-04 BIENNIAL STATEMENT 2013-03-01
110331003266 2011-03-31 BIENNIAL STATEMENT 2011-03-01
090304002255 2009-03-04 BIENNIAL STATEMENT 2009-03-01
070327002857 2007-03-27 BIENNIAL STATEMENT 2007-03-01
050405002249 2005-04-05 BIENNIAL STATEMENT 2005-03-01

USAspending Awards / Contracts

Procurement Instrument Identifier:
NNX17CL50P
Link:
View Award on USAspending website
Award Or Idv Flag:
AWARD
Award Type:
PURCHASE ORDER
Action Obligation:
125000.00
Base And Exercised Options Value:
125000.00
Base And All Options Value:
125000.00
Awarding Agency Name:
National Aeronautics and Space Administration
Performance Start Date:
2017-06-09
Description:
IGF::OT::IGF CLEAR SCIENCE CORP. PROPOSES TO DEVELOP AND DEMONSTRATE COMPUTATIONAL FLUID DYNAMICS (CFD)-BASED SOFTWARE FOR DESIGNING AND EVALUATING ACTIVE FLOW CONTROL (AFC) SYSTEMS ON AIRCRAFT. THE SOFTWARE WILL FACILITATE THE IDENTIFICATION OF OPTIMAL TYPES OF ACTUATION AND THEIR LOCATIONS, WILL SUPPORT VIRTUAL FLIGHT TESTING WITH BOTH OPEN- AND CLOSED-LOOP CONTROL SYSTEMS, AND WILL ENABLE QUANTITATIVE TRADE STUDIES THAT COMPARE PERFORMANCE ENHANCEMENTS THROUGH AFC TO THE COSTS OF CONTROL. IN SUBSONIC, TRANSONIC, AND SUPERSONIC APPLICATIONS, AFC SYSTEMS CAN IMPROVE AIR VEHICLE PERFORMANCE BY REDUCING AND/OR ELIMINATING SEPARATION AND INCREASING CIRCULATION---RESULTING IN SMALLER CONTROL SURFACES, LESS WEIGHT, LOWER DRAG, AND LESS FUEL CONSUMPTION. MANY AFC APPLICATIONS INVOLVE HIGHLY UNSTEADY FLOW DYNAMICS WITH TURBULENCE, UNSTEADY SHOCKS, SEPARATION, AND AEROSERVOELASTICITY INTERACTING IN COMPLEX WAYS THAT RENDER OPEN-LOOP SYSTEMS EITHER INEFFECTIVE OR TOO COSTLY IN TERMS OF ENERGY, WEIGHT, AND VOLUME. FOR THIS REASON, CLOSED-LOOP AFC SYSTEM DESIGN WILL BE A CRITICAL AREA OF FOCUS IN THE PROPOSED PROJECT. COMPONENTS OF CLOSED-LOOP SYSTEMS INCLUDE DYNAMICAL AND MEASUREMENT-BASED STATE ESTIMATORS, REGULATORS, AND COMPENSATORS. THE PROPOSED AFC SYSTEM DESIGN AND ANALYSIS SOFTWARE WILL BE DEVELOPED USING THE X-56 EXPERIMENTAL AIRCRAFT AS A DEMONSTRATION PLATFORM, A LONG-RANGE, HIGHLY FLEXIBLE AIR VEHICLE CURRENTLY UNDER DEVELOPMENT AT THE NASA ARMSTRONG FLIGHT TEST CENTER.
Naics Code:
541712: RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
Product Or Service Code:
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
Procurement Instrument Identifier:
NNX17CD02C
Link:
View Award on USAspending website
Award Or Idv Flag:
AWARD
Award Type:
DEFINITIVE CONTRACT
Action Obligation:
0.00
Base And Exercised Options Value:
0.00
Base And All Options Value:
0.00
Awarding Agency Name:
National Aeronautics and Space Administration
Performance Start Date:
2017-05-01
Description:
IGF::OT::IGF CLEAR SCIENCE CORP. PROPOSES TO DEVELOP AND DEMONSTRATE COMPUTATIONAL FLUID DYNAMICS (CFD)-BASED, REDUCED-ORDER AEROSERVOELASTICITY MODELING AND SIMULATION TECHNOLOGY FOR FAST AND ACCURATE PREDICTIONS OF NONLINEAR FLIGHT DYNAMICS, ENABLING REAL-TIME, PILOTED AND UNPILOTED FLIGHT SIMULATIONS AND PROVIDING A TOOL TO DESIGN FLIGHT CONTROLLERS FOR HIGHLY FLEXIBLE, LIGHTWEIGHT AIRCRAFT. PHYSICS-BASED, REDUCED-ORDER MODELS (ROMS) WILL BE DEVELOPED AND DEMONSTRATED WITH DATA FROM CFD MODELS OF THE X-56, AN EXPERIMENTAL AIRCRAFT THAT NASA AND THE U. S. AIR FORCE ARE USING TO TEST SYSTEMS FOR FLUTTER SUPPRESSION AND GUST-LOAD ALLEVIATION. EXTENDED RANGE AND LOW FUEL CONSUMPTION THROUGH LIGHTWEIGHT MATERIALS AND LARGE WING SPANS (HIGH LIFT-TO-DRAG RATIOS) ARE THE DRIVERS IN NEXT-GENERATION AIRCRAFT LIKE THE X-56, BUT THESE ATTRIBUTES CREATE CHALLENGES IN MAINTAINING FLIGHT SAFETY, RIDE QUALITY, AND LONG-TERM STRUCTURAL DURABILITY. THE DEVELOPMENT OF FLIGHT CONTROLLERS THAT CAN ACTIVELY MANAGE AEROSERVOELASTIC EFFECTS (BODY-FREEDOM FLUTTER, CONTROL REVERSAL, GUST LOADING) WITHOUT COMPROMISING SAFETY AND AERODYNAMIC PERFORMANCE IS A KEY OBJECTIVE OF BOTH THE X-56 PROGRAM AND THE PROPOSED PROJECT. THROUGH THE PROPOSED TECHNOLOGY, NONLINEAR, AEROSERVOELASTIC ROMS CAN BE COUPLED TO OTHER COMPONENTS OF A FLIGHT SIMULATOR (SIX-DEGREES-OF-FREEDOM FLIGHT MECHANICS MODELS AND CONTROL SOFTWARE) TO IMPROVE THE FIDELITY OF SIMULATIONS THAT SUPPORT CONTROLLER DESIGN FOR A WIDE RANGE OF OPERATING CONDITIONS.
Naics Code:
541712: RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
Product Or Service Code:
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)
Procurement Instrument Identifier:
NNX16CD19P
Link:
View Award on USAspending website
Award Or Idv Flag:
AWARD
Award Type:
PURCHASE ORDER
Action Obligation:
125000.00
Base And Exercised Options Value:
125000.00
Base And All Options Value:
125000.00
Awarding Agency Name:
National Aeronautics and Space Administration
Performance Start Date:
2016-06-10
Description:
IGF::OT::IGF CLEAR SCIENCE CORP. PROPOSES TO DEVELOP AND DEMONSTRATE COMPUTATIONAL FLUID DYNAMICS (CFD)-BASED, REDUCED-ORDER AEROSERVOELASTICITY MODELING AND SIMULATION TECHNOLOGY FOR FAST AND ACCURATE PREDICTIONS OF NONLINEAR FLIGHT DYNAMICS, ENABLING REAL-TIME, PILOTED AND UNPILOTED FLIGHT SIMULATIONS AND PROVIDING A TOOL TO DESIGN FLIGHT CONTROLLERS FOR HIGHLY FLEXIBLE, LIGHTWEIGHT AIRCRAFT. PHYSICS-BASED, REDUCED-ORDER MODELS (ROMS) WILL BE DEVELOPED AND DEMONSTRATED WITH DATA FROM CFD MODELS OF THE X-56, AN EXPERIMENTAL AIRCRAFT THAT NASA AND THE U. S. AIR FORCE ARE USING TO TEST SYSTEMS FOR FLUTTER SUPPRESSION AND GUST-LOAD ALLEVIATION. EXTENDED RANGE AND LOW FUEL CONSUMPTION THROUGH LIGHTWEIGHT MATERIALS AND LARGE WING SPANS (HIGH LIFT-TO-DRAG RATIOS) ARE THE DRIVERS IN NEXT-GENERATION AIRCRAFT LIKE THE X-56, BUT THESE ATTRIBUTES CREATE CHALLENGES IN MAINTAINING FLIGHT SAFETY, RIDE QUALITY, AND LONG-TERM STRUCTURAL DURABILITY. THE DEVELOPMENT OF FLIGHT CONTROLLERS THAT CAN ACTIVELY MANAGE AEROSERVOELASTIC EFFECTS (BODY-FREEDOM FLUTTER, CONTROL REVERSAL, GUST LOADING) WITHOUT COMPROMISING SAFETY AND AERODYNAMIC PERFORMANCE IS A KEY OBJECTIVE OF BOTH THE X-56 PROGRAM AND THE PROPOSED PROJECT. THROUGH THE PROPOSED TECHNOLOGY, NONLINEAR, AEROSERVOELASTIC ROMS CAN BE COUPLED TO OTHER COMPONENTS OF A FLIGHT SIMULATOR (SIX-DEGREES-OF-FREEDOM FLIGHT MECHANICS MODELS AND CONTROL SOFTWARE) TO IMPROVE THE FIDELITY OF SIMULATIONS THAT SUPPORT CONTROLLER DESIGN FOR A WIDE RANGE OF OPERATING CONDITIONS.
Naics Code:
541712: RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
Product Or Service Code:
AR11: R&D- SPACE: AERONAUTICS/SPACE TECHNOLOGY (BASIC RESEARCH)

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Date of last update: 30 Mar 2025

Sources: New York Secretary of State

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