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Company Information:

Company Name:
SOFTWARE & ENGINEERING ASSOC., INC.
Address:
1802 N. Carson Street
Suite 200
Carson City, NV 89701-1238
Phone:
(775) 882-1966
URL:
N/A
EIN:
953015605
DUNS:
83152975
Number of Employees:
8
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 $788,854.00 9
SBIR Phase II $3,879,675.00 6
STTR Phase I $199,792.00 2

Award List:

Automated 3-D Acoustic Stability,/ Grain Design Analysis

Award Year / Program / Phase:
1996 / SBIR / Phase I
Award Amount:
$69,988.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Stuart Dunn
Abstract:
N/a

Automated 3-D Acoustic Stability,/ Grain Design Analysis

Award Year / Program / Phase:
1997 / SBIR / Phase II
Award Amount:
$599,948.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Stuart Dunn
Abstract:
The novel approach described in this proposal has the potential to allow designers of solid propellant rocket motors to assess the impact of their design choices on motor stability during the preliminary design phase of the motor development cycle. The potential cost savings to the government and… More

Innovative Sensor Technologies for In-Situ Air and Ocean Sampling under Extreme Conditions

Award Year / Program / Phase:
2001 / SBIR / Phase I
Award Amount:
$69,951.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Douglas Coats, President
Abstract:
Chemical kinetics based solid propellant combustion predictive capabilities have developed to the point where it is possible to compute combustion properties of solid propellants. Specifically burning rates over a range of pressures and temperatures.This capability will reduce the time, effort, and… More

An Innovative Method of NOX Reduction Through Fuel Additives for the UEET Program

Award Year / Program / Phase:
2002 / SBIR / Phase I
Award Amount:
$99,252.00
Agency:
NASA
Principal Investigator:
Homayun Navaz
Abstract:
The opportunity addressed in this proposal is to transfer a fuel-additive technology developed for NOx and particulate matter reduction in diesel fuels, to applications in ultra-efficient jet engine fuels, with no reduction in performance and power output of the engine. The innovation is based on a… More

Modeling of Composite Solid Propellant Combustion

Award Year / Program / Phase:
2002 / SBIR / Phase II
Award Amount:
$450,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Douglas E. Coats, President
Abstract:
Chemical kinetics based solid propellant combustion predictive capabilities have developed to the point where it is possible to compute combustion properties of solid propellants. Specifically, burning rates over a range of pressures and temperatures.This capability will reduce the time, effort,… More

Modeling High-Temperature Erosive Gas Flow to Support Barrel Erosion Reduction Concept Modeling for Fire Support Gun Application

Award Year / Program / Phase:
2002 / SBIR / Phase II
Award Amount:
$749,936.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Stuart S. Dunn, Senior Engineer
Abstract:
"New requirements for modern gun systems have greatly increasedthe propellant flame temperature and reactivity of the combustionproducts. As a result, thermochemical erosion can greatlyreduced the service life of the gun tubes in these systems.Coatings and liners have been used to mitigate erosion,… More

Modeling High-Temperature Erosive Gas Flow to Support Barrel Erosion Reduction Concept Modeling for Fire Support Gun Application

Award Year / Program / Phase:
2002 / SBIR / Phase I
Award Amount:
$99,925.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Stuart S. Dunn, Senior Research Engineer
Abstract:
"New requirements for modern gun systems have greatly increased the propellant flame temperature and reactivity of the combustion products. As a result, thermochemical erosion can greatly reduced the service life of the gun tubes in these systems.Coatings and liners have been used to mitigate… More

Nonlinear Combustion Stability Prediction of Solid Rocket Motors

Award Year / Program / Phase:
2002 / SBIR / Phase I
Award Amount:
$99,915.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Jonathan C. French, Senior Engineer
Abstract:
"Software & Engineering Associates, Inc., proposes to develop a new tool to analyze solid rocket motor combustion stability which will predict for an unstable motor the combustion chamber's maximum over-pressurization. When a rocket motor experiencescombustion instability, it often does not… More

Non-Linear Combustion Stability Prediction of Solid Rocket Motors

Award Year / Program / Phase:
2002 / SBIR / Phase II
Award Amount:
$599,866.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Jonathan C. French, Senior Engineer
Abstract:
"Solid rocket motors are subject to combustion stability problemswhen the interior combustion processes interact with thecombustion chamber's acoustic modes, resulting in large pressureamplitude fluctuations. While the initial excitation process canbe predicted using linear analysis, the… More

Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components

Award Year / Program / Phase:
2003 / SBIR / Phase I
Award Amount:
$99,947.00
Agency / Branch:
DOD / OSD
Principal Investigator:
Stuart S. Dunn, Senior Research Engineer
Abstract:
Design of a high performance hydrocarbon liquid rocket engine (LRE) requires a thorough understanding of the heat transfer and cooling requirements of LRE's. An efficient cooling system is crucial in extending engine life and minimizing pumping power. Itis essential to be able to accurately… More

Advanced Cooling Techniques for Hydrocarbon Liquid Rocket Engine Components

Award Year / Program / Phase:
2004 / SBIR / Phase II
Award Amount:
$749,973.00
Agency / Branch:
DOD / OSD
Principal Investigator:
Stuart S. Dunn, Senior Research Engineer
Abstract:
Liquid rocket engines may be run for repeatedly over extended periods of time, requiring active cooling. An efficient means of cooling LRE nozzles involves using the liquid fuel or oxidizer itself to provide the cooling, often referred to as regenerative cooling. SEA's liquid rocket combustion… More

Innovative Predictive Model for Determining Bore Erosion

Award Year / Program / Phase:
2006 / SBIR / Phase I
Award Amount:
$69,997.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Stuart S. Dunn, Senior Research Engineer
Abstract:
New requirements for modern gun systems have greatly increased the propellant flame temperature and reactivity of the combustion products. As a result, thermochemical erosion can greatly reduced the service life of the gun tubes in these systems. Coatings, liners, additives, and deterred… More

Aluminum Agglomeration and Trajectory in Solid Rocket Motors

Award Year / Program / Phase:
2006 / STTR / Phase I
Award Amount:
$99,819.00
Agency / Branch:
DOD / USAF
Principal Investigator:
E. C. Hylin, Senior Engineer
Research Institution:
BRIGHAM YOUNG UNIV.
RI Contact:
Merrill Beckstead
Abstract:
The demand for higher performance rocket motors at a reduced cost requires continuous improvements in understanding and controlling propellant combustion. Numerous examples are available where seemingly minor modifications and improvements to existing solid rocket systems have caused previously… More

STTR Phase I: Multi-Dimensional Hydrodynamic Stability Analysis Tool for Solid Rocket Motors

Award Year / Program / Phase:
2006 / STTR / Phase I
Award Amount:
$99,973.00
Agency:
NSF
Principal Investigator:
Research Institution:
Univ of TN Space Inst
RI Contact:
Joseph Majdalani
Abstract:
This Small Business Technology Transfer (STTR) Phase I project is to determine the feasibility of developing a hydrodynamic combustion stability analysis design tool for rockets, gas turbines, and large engines. As combustors are run at leaner mixture ratios to avoid NOx pollutant issues, vortex… More

Advanced Rocket Propulsion Technologies

Award Year / Program / Phase:
2006 / SBIR / Phase I
Award Amount:
$99,909.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Jonathan C. French, Senior Research Engineer
Abstract:
A modeling and experimental program is proposed with the goal of reducing the mean size of metal oxide droplets in the exhaust of solid propellant rocket motors (SRMs). The proposed effort looks at all aspects of metal combustion and discrete phase dynamics which occur in SRMs and offers approaches… More

Innovative Predictive Model for Determining Bore Erosion

Award Year / Program / Phase:
2008 / SBIR / Phase II
Award Amount:
$729,952.00
Agency / Branch:
DOD / ARMY
Principal Investigator:
Stuart S. Dunn, Vice Pres/Sr Research Eng
Abstract:
New requirements for modern gun systems have greatly increased the propellant flame temperature and reactivity of the combustion products. As a result, thermochemical erosion can greatly reduced the service life of the gun tubes in these systems. Coatings, liners, additives, and deterred… More

Acoustic Stability Prediction In Solid Rocket Motors

Award Year / Program / Phase:
2010 / SBIR / Phase I
Award Amount:
$79,970.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Anthony Dang, Principal Research Scient
Abstract:
The ability for engineers to assess the impact of their preliminary design of solid rocket motor (SRM) performance and combustion stability is the focus of this proposal. The SRMs of the future will be designed for increased performance. Since ballistic excursions, instabilities, and sporadic forces… More