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Company Information:

Company Name:
Aero-plasma, Inc.
Address:
23974 Craftsman Rd.
Calabasas, CA 91302
Phone:
N/A
URL:
N/A
EIN:
N/A
DUNS:
N/A
Number of Employees:
7
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 $336,025.00 6
SBIR Phase II $491,000.00 1

Award List:

IGNITION AND FLAME FRONT SUSTENANCE OF NAVY AIRCRAFT JET PROPULSION SYSTEMS BY USE OF MICROWAVE IRRADIATION

Award Year / Program / Phase:
1987 / SBIR / Phase I
Award Amount:
$49,403.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
William P Peschel
Abstract:
N/a

AN ADVANCED METHOD FOR STAGNATION ENTHALPY ADDITION AND RECONSTRUCTION IN HYPERSONIC WIND TUNNEL TESTING

Award Year / Program / Phase:
1989 / SBIR / Phase I
Award Amount:
$49,906.00
Agency / Branch:
DOD / USAF
Principal Investigator:
William P Peschel
Abstract:
The characterization of flight behavior in the high-hyersonic domain (mach 5-20) and at altitudes from 1-3x10(5) feet (30-100 km) has great relevance for the design and development of the aotv, nasp, and hypersonic reentry vehicles. deficiencies in our present knowledge and understanding of the… More

IGNITION AND FLAME FRONT SUSTENANCE OF NAVY AIRCRAFT JET PROPULSION SYSTEMS BY USE OF MICROWAVE IRRADIATION

Award Year / Program / Phase:
1990 / SBIR / Phase II
Award Amount:
$491,000.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
William P Peschel
Abstract:
An innovative method for ignition and flame front sustenance of jet engine aircraft propulsion systems is proposed. this method utilizes the interaction of controlled and concentrated microwave energy with the fuel-air mixture in the combustion chamber or afterburner. the highly efficient microwave… More

NONINTRUSIVE METHOD FOR DETERMINING PLASMA PROFILES IN HYPERSONIC BOUNDARY LAYERS

Award Year / Program / Phase:
1990 / SBIR / Phase I
Award Amount:
$49,833.00
Agency / Branch:
DOD / USAF
Principal Investigator:
William P Peschel
Abstract:
Comprises in wind tunnel operational parameters, relative to actual atmospheric flight, and inadequacines in numerical simulations indicate the requirement for a nonintrusive diagnostic technique which can enable profiles of key plasma boundary layer parameters (e.e., electron density and electron… More

TECHNICAL EVALUATION OF X-RAY SIMULATION PLASMA OPENING SWITCH AND OTHER KEY COMPONENT PERFORMANCE AND SYSTEM INTEGRATIONS

Award Year / Program / Phase:
1990 / SBIR / Phase I
Award Amount:
$49,869.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Dr Jacob L Sperling
Abstract:
The proposed effort is intended to provide in depth technological support to the arnold engineering development center (aedc) for the interpretation and evaluation of the relation between the major pulse forming devices in the advanced pulsepower systems used in conjunction with inductive… More

Microwave Powered Plasma On-Orbir Thruster System Using a Non-Resonant Plasma Generator

Award Year / Program / Phase:
1994 / SBIR / Phase I
Award Amount:
$59,976.00
Agency / Branch:
DOD / USAF
Principal Investigator:
William P. Peschel
Abstract:
An innovative Microwave-Powered Plasma Thruster concept for On-Orbit application is proposed based on its significant ISP magnitude advantages over the electric arcjet thrusters attained by reduction of inherent arcjet energy losses resulting as a consequence of the pinch plasma arc used for heating… More

Monopropellant Hydrogen Plasma Ignition System for Hydrogen Rocket Engine

Award Year / Program / Phase:
1996 / SBIR / Phase I
Award Amount:
$77,038.00
Agency / Branch:
DOD / USAF
Principal Investigator:
William P. Peschel
Abstract:
An innovative Microwave-Powered Monopropellant Hydrogen Plasma Ignition System for hydrogen fueled rocket engines, which develops a plasma using only the hydrogen feed gas to the igniter, is proposed to replace current enhanced spark or torch igniters which require the use of a pre-mixed quantity of… More