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Company Information:

Company Name:
Science and Technology Applications, LLC
Address:
530 New Los Angeles Avenue, Suite115
# 122
Moorpark, CA 93021-
Phone:
(805) 529-3800
URL:
EIN:
202063450
DUNS:
172773272
Number of Employees:
5
Woman-Owned?:
Yes
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 $399,884.00 3
SBIR Phase II $739,572.00 1
STTR Phase I $399,836.00 4
STTR Phase II $1,499,744.00 2

Award List:

All-Nitrogen or High-Nitrogen Compounds as High Energy Density Materials

Award Year / Program / Phase:
2006 / STTR / Phase II
Award Amount:
$749,931.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Karl O. Christe, Sr. Research Scientist
Research Institution:
UNIV. OF SOUTHERN CALIFORNIA
RI Contact:
Ralf Haiges
Abstract:
During Phase II of the proposed program, Science and Technology Applications, LLC, proposes to prepare novel energetic materials identified during Phase I as potential targets. Therefore, the objectives of the proposed work in Phase II are (i) the development of synthetic methods for the preparation… More

Combustion Stability Innovations for Liquid Rocket

Award Year / Program / Phase:
2006 / STTR / Phase I
Award Amount:
$99,982.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Tedi Ohanian, CEO/Chief Technical Officer
Research Institution:
GEORGIA INSTITUTE OF TECHNOLOGY
RI Contact:
Ben Zinn
Abstract:
Combustion instability in liquid rocket engines (LREs) has manifested in nearly all LRE development programs. While the driving mechanisms of combustion instability are vast and coupled, in all instances, the net result is significant cost and schedule over-runs. In today's business environment,… More

Environmentally-Benign Oxidizers for Propulsion

Award Year / Program / Phase:
2006 / STTR / Phase I
Award Amount:
$99,971.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Karl Christe, Principal Investigator
Research Institution:
UNIV. OF SOUTHERN CALIFORNIA
RI Contact:
Robert Bau
Abstract:
Ammonium perchlorate (AP) is the most commonly used oxidizing ingredient in solid propellant formulations. It carries a sufficient excess of oxygen to allow for the combustion of the required binder and added metal, such as aluminum. The major drawback of AP is its chlorine content which results in… More

Innovative Deep Throttling, High Performance Injector Concept

Award Year / Program / Phase:
2007 / STTR / Phase I
Award Amount:
$99,904.00
Agency:
NASA
Principal Investigator:
Tedi E. Ohanian, Principal Investigator
Research Institution:
Georgia Tech Research Corporation
RI Contact:
N/A
Abstract:
Science and Technology Applications, LLC's (STA) vision for a versatile space propulsion system is a highly throttleable, high performance, and cost effective Liquid Oxygen/Hydrogen engine utilizing innovative design and manufacturing processes to simultaneously meet NASA's Space Exploration… More

Environmentally-Benign Oxidizers for Propulsion

Award Year / Program / Phase:
2007 / STTR / Phase II
Award Amount:
$749,813.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Karl Christe, Principal Investigator
Research Institution:
UNIV. OF SOUTHERN CALIFORNIA
RI Contact:
Robert Bau
Abstract:
During Phase II of the proposed program, Science and Technology Applications, LLC (STA), proposes to find a green replacement for ammonium perchlorate (AP). During Phase I of this program, the novel tetranitroborate, B(NO2)4-, anion, was identified as a potential high-oxygen carrier. Its combination… More

Variable Thrust and Non-Toxic Liquid Propulsion for Mission Flexibility

Award Year / Program / Phase:
2008 / SBIR / Phase I
Award Amount:
$99,995.00
Agency / Branch:
DOD / OSD
Principal Investigator:
Tedi Ohanian, CEO/Chief Technical Officer
Abstract:
Our vision for the next generation missile propulsion is a flexible and non-toxic system using HAN and a storable fuel candidate, offering variable thrust with a high degree of mission tailoring. Additionally, such system will be capable of rapid transients to enable pulsed propulsion for tactical… More

High Performance Cooling Methods for Liquid Rocket Engines

Award Year / Program / Phase:
2012 / SBIR / Phase I
Award Amount:
$149,974.00
Agency:
DOD
Principal Investigator:
Tedi Ohanian, CEO/Chief Technical Officer – (805) 529-3800
Abstract:
ABSTRACT: To meet the goals for future generation Air Force LOX/Hydrocarbon booster engines, improvements must be made in performance, operability, reusability, reliability, and cost. To date, operational LOX/hydrocarbon engines have used the fuel as the thrust chamber assembly (TCA) regenerative… More

High Performance Cooling Methods for Liquid Rocket Engines

Award Year / Program / Phase:
2013 / SBIR / Phase II
Award Amount:
$739,572.00
Agency:
DOD
Principal Investigator:
Tedi Ohanian, CEO/Chief Technical Offic – (805) 529-3800
Abstract:
ABSTRACT: To meet the goals for future generation Air Force LOX/Hydrocarbon booster engines, improvements must be made in performance, operability, reusability, reliability, and cost. To date, operational LOX/hydrocarbon engines have used the fuel as the thrust chamber assembly (TCA) regenerative… More

Lowest Lifecycle Cost (LLC) Expendable Launch Vehicles

Award Year / Program / Phase:
2014 / SBIR / Phase I
Award Amount:
$149,915.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Tedi Ohanian, CEO/Chief Technical Officer – (805) 529-3800
Abstract:
ABSTRACT: To meet the goals of future generation of ELVs, significant improvements must be made in cost. Current expendable launch vehicles are designed using an optimum performance methodology. Recent studies and technology demonstrations suggest that designing to minimum cost may have life cycle… More