USA flag logo/image

An Official Website of the United States Government

Company Information:

Company Name:
AEROGAGE CORP.
Address:
7 Matthew Lane
Sterling, MA 01564
Phone:
(978) 422-8224
URL:
N/A
EIN:
43246653
DUNS:
799543744
Number of Employees:
4
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $149,718.00 3
SBIR Phase II $599,754.00 1

Award List:

N/A

Award Year / Program / Phase:
2000 / SBIR / Phase I
Award Amount:
$69,718.00
Agency:
NASA
Principal Investigator:
Abstract:
N/a

Capacitance-Based Turbine Blade Vibration Monitor

Award Year / Program / Phase:
2001 / SBIR / Phase I
Award Amount:
$0.00
Agency:
NASA
Principal Investigator:
Abstract:
Prevention of catastrophic failure of engine components is a major goal to the subtopic. Catastrophic failures of turbine engines are often caused by vibration-induced compressor and fan blade fatigue fractures. Existing capacitance systems have been unable to accurately measure blade vibration due… More

Capacitance-Based Turbine Blade Vibration Monitor

Award Year / Program / Phase:
2001 / SBIR / Phase II
Award Amount:
$599,754.00
Agency:
NASA
Principal Investigator:
Abstract:
Prevention of catastrophic failure of engine components is a major goal to the subtopic. Catastrophic failures of turbine engines are often caused by vibration-induced compressor and fan blade fatigue fractures. Existing capacitance systems have been unable to accurately measure blade vibration due… More

High-Resolution Non-Intrusive-Stress-Measurement-System (NSMS) Sensor

Award Year / Program / Phase:
2006 / SBIR / Phase I
Award Amount:
$80,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Abstract:
The goal of this project is to develop a magnetic sensor that will accurately detect the time-of-arrival of turbine engine blades from outside the engine case and from standoff distances from the first stage fan via the inlet aperture, with the intent of achieving performance comparable to the… More