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Company Information:

Company Name:
Irvine Technology Gp Inc.
Address:
9 St Maxime
Laguna Niguel, CA 92677
Phone:
N/A
URL:
N/A
EIN:
N/A
DUNS:
N/A
Number of Employees:
5
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 $126,536.00 2
SBIR Phase II $1,157,062.00 2

Award List:

AUTONOMOUS CONTROL SYSTEM FOR LOW-THRUST ORBITAL TRANSFER VEHICLE (OTV) FOR GLOBAL POSITIONING SYSTEM (GPS)

Award Year / Program / Phase:
1987 / SBIR / Phase I
Award Amount:
$58,360.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Ronald E Oglevie
Abstract:
N/a

AUTONOMOUS CONTROL SYSTEM FOR LOW-THRUST ORBITAL TRANSFER VEHICLE (OTV) FOR GLOBAL POSITIONING SYSTEM (GPS)

Award Year / Program / Phase:
1988 / SBIR / Phase II
Award Amount:
$700,000.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Ronald E Oglevie
Abstract:
The proposed project will develop innovative techniques for low-cost control of the attitude and engine firing of the electric orbital transfer vehicle (eotv) during its spiral orbit transfer mission. the eotv promises the ability to deliver gps replenishment satellites to their operational orbits… More

MICROCOMPUTER-BASED EARTH-TO-ORBIT TRAJECTORY OPTIMIZATION PROGRAM

Award Year / Program / Phase:
1989 / SBIR / Phase I
Award Amount:
$68,176.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Ronald E Oglevie
Abstract:
N/a

MICROCOMPUTER-BASED EARTH-TO-ORBIT TRAJECTORY OPTIMIZATION PROGRAM

Award Year / Program / Phase:
1991 / SBIR / Phase II
Award Amount:
$457,062.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Ronald E Oglevie
Abstract:
The primary objective is the development of an earth-to-orbit trajectory optimization program capable of accommodating air breathing propulsion and suitable for preliminary design analysis. rapid execution and ease-of-use are required. a dual mode approach is proposed with the following features:… More