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Company Information:

Company Name:
Comet Technology Corporation
Address:
1796 Stonebridge Drive North
Ann Arbor, MI 48108-2051
Phone:
(734) 973-1600
URL:
EIN:
200454824
DUNS:
136770703
Number of Employees:
3
Woman-Owned?:
No
Minority-Owned?:
Yes
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 $531,780.00 6
SBIR Phase II $1,197,828.00 2
STTR Phase I $99,719.00 1
STTR Phase II $749,452.00 1

Award List:

Vehicle Interior Noise Prediction Using Energy Finite Element Analysis

Award Year / Program / Phase:
2004 / SBIR / Phase I
Award Amount:
$69,800.00
Agency:
NASA
Principal Investigator:
Satha T. Raveendra, Principal Investigator
Abstract:
Prediction and enhancement of vehicle interior noise due to high frequency excitation, based on computer simulation, allows the application of the technology at the early stage of design process thereby improving the quality and reducing the cost. Traditionally, Statistical Energy Analysis (SEA) has… More

Identification of Turbomachinery Noise Sources Using Acoustical Holography

Award Year / Program / Phase:
2004 / SBIR / Phase I
Award Amount:
$69,752.00
Agency:
NASA
Principal Investigator:
Satha Raveendra, Principal Investigator
Abstract:
Evaluation and enhancement of the acoustical performance of turbomachinery requires knowledge of the acoustic sources. However, the noise generation mechanisms associated with turbomachinery are complex and as result it is not easy to identify these noise sources. The development of an integrated… More

Vehicle Interior Noise Prediction Using Energy Finite Element Analysis

Award Year / Program / Phase:
2005 / SBIR / Phase II
Award Amount:
$598,181.00
Agency:
NASA
Principal Investigator:
Satha Raveendra, Principal Investigator
Abstract:
It is proposed to develop and implement a computational technique based on Energy Finite Element Analysis (EFEA) for interior noise prediction of advanced aerospace vehicles that will expand NASA's noise prediction capability at the early stage of design process. In many situations, aerospace… More

Identification and Reduction of Turbomachinery Noise

Award Year / Program / Phase:
2006 / SBIR / Phase I
Award Amount:
$69,272.00
Agency:
NASA
Principal Investigator:
Satha Raveendra, Principal Investigator
Abstract:
Noise has become a primary consideration in the design and development of many products, particulary in aerospace, automotive and consumer product industries. Communities near airports are often exposed to high noise levels due to low flying aircraft in the takeoff and landing phases of fligh and… More

Identification and Reduction of Turbomachinery Noise

Award Year / Program / Phase:
2007 / SBIR / Phase II
Award Amount:
$599,647.00
Agency:
NASA
Principal Investigator:
S. T. Raveendra, Principal Investigator
Abstract:
Communities near airports are often exposed to high noise levels due to low flying aircraft in the takeoff and landing phases of flight. Propulsion source noise is the major contributor to the overall noise level. The noise generation mechanisms for a typical turbofan engine are complicated, which… More

Failure Initiation Predictors for Reliability-Based Design of Hybrid Composite Materials

Award Year / Program / Phase:
2009 / STTR / Phase I
Award Amount:
$99,719.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Research Institution:
UNIV. OF MICHIGAN
RI Contact:
Krista L. Campeau
Abstract:
This proposal is concerned with the development of a novel failure initiation and progressive failure analysis (PFA) modeling method for advanced composite structures. The laminate is modeled as a collection of degrading lamina within the framework of lamination theory and executed using user… More

Hybrid Element Method for Mid-Frequency Vibroacoustic Analysis

Award Year / Program / Phase:
2009 / SBIR / Phase I
Award Amount:
$99,930.00
Agency:
NASA
Principal Investigator:
S. T. Raveendra, Principal Investigator
Abstract:
In many situations, aerospace structures are subjected to a wide frequency spectrum of mechanical and/or acoustic excitations and therefore, there is a need for the development of numerical modeling techniques that are applicable for the resolution of dynamic response of complex systems spanning the… More

Failure Initiation Predictors for Reliability-Based Design of Hybrid Composite Materials

Award Year / Program / Phase:
2010 / STTR / Phase II
Award Amount:
$749,452.00
Agency / Branch:
DOD / USAF
Principal Investigator:
S. T. Raveendra, President
Research Institution:
The University of Michigan
RI Contact:
Krista L. Campeau
Abstract:
ABSTRACT: This proposal is concerned with the development of a novel failure initiation and progressive failure analysis modeling method for advanced composite structures, including the analysis of selected structural joints utilizing a statistically based micromechanics model embedded in a 3D… More

Hybrid Element Method for Compsoite Structures Subjected to Boundary Layer Loading

Award Year / Program / Phase:
2011 / SBIR / Phase I
Award Amount:
$98,183.00
Agency:
NASA
Principal Investigator:
S. T. Raveendra, Principal Investigator
Abstract:
In many situations, aerospace structures are subjected to a wide frequency spectrum of mechanical and/or acoustic excitations and therefore, there is a need for the development of numerical modeling techniques that are applicable for the resolution of dynamic response of complex systems spanning the… More

Substrucured, Meshless and Parametric Modeling of Vibroacoustic Systems

Award Year / Program / Phase:
2013 / SBIR / Phase I
Award Amount:
$124,843.00
Agency:
NASA
Principal Investigator:
Satha Raveendra, Principal Investigator
Abstract:
Aerospace structures are often subjected to a broad spectrum of mechanical and/or aerodynamic excitations and, therefore, there is a real need for the development of a modeling technique which can be used for the vibroacoustic analysis, with high fidelity and adequate spatial and spectral… More