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Company Information:

Company Name:
Software & Engineering Associa
Address:
1000 E William St - Ste 200
Carson City, NV 89701
Phone:
N/A
URL:
N/A
EIN:
N/A
DUNS:
N/A
Number of Employees:
10
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 $99,963.00 2
SBIR Phase II $894,222.00 2

Award List:

THE CHEMICAL KINETICS OF LOX/HYDROCARBON COMBUSTION

Award Year / Program / Phase:
1989 / SBIR / Phase I
Award Amount:
$49,989.00
Agency:
NASA
Principal Investigator:
Gary R Nickerson
Abstract:
N/a

THE CHEMICAL KINETICS OF LOX/HYDROCARBON COMBUSTION

Award Year / Program / Phase:
1990 / SBIR / Phase II
Award Amount:
$390,031.00
Agency:
NASA
Principal Investigator:
Gary R Nickerson
Abstract:
Analytical methods and computer software are to be developed for characterizing the chemical kinetic mechanisms that control lox/hydrocarbon combustion in rocket engines. critical areas of technology are to be identified. an innovative and highly general method will beapplied to model lox/rp-1… More

COMBUSTION PROCESSES IN SPACE STORABLE LIQUID ROCKET ENGINES

Award Year / Program / Phase:
1990 / SBIR / Phase I
Award Amount:
$49,974.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Gary R Nickerson
Abstract:
N/a

COMBUSTION PROCESSES IN SPACE STORABLE LIQUID ROCKET ENGINES

Award Year / Program / Phase:
1991 / SBIR / Phase II
Award Amount:
$504,191.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Gary R Nickerson
Abstract:
The exhaust from nto/mmh fuel rich gas generators (gg) are known to contain a large fraction of ammonia. this phenomenon makes it possible to actively cool a rocket nozzle wall using the endothermic decomposition of ammonia. a realistic analysis of this combustion process is to be developed which… More