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Company Information:

Company Name:
HYPERSONICS
Address:
164 FERNE COURT
PALO ALTO, CA 94306 0460
Phone:
(650) 856-3013
URL:
N/A
EIN:
N/A
DUNS:
178051900
Number of Employees:
4
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 $488,496.00 7
SBIR Phase II $2,139,563.00 4

Award List:

COMPUTATIONAL TOOL FOR ANTENNA WINDOW ABLATION

Award Year / Program / Phase:
1987 / SBIR / Phase I
Award Amount:
$65,405.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Paul J Conti
Abstract:
N/a

COMPUTATIONAL TOOL FOR ANTENNA WINDOW ABLATION

Award Year / Program / Phase:
1989 / SBIR / Phase II
Award Amount:
$439,791.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Paul J Conti
Abstract:
Current shape-change computer codes used to predict antenna window (aw) erosion place emphasis on the physics of the ablation/melting process. one of their weakest areas is the calculation of the heat input from the hypersonic flow. this proposal addresses the adaptation of an advanced navier-stokes… More

ADVANCED AEROTHERMOCHEMISTRY ALGORITHM

Award Year / Program / Phase:
1990 / SBIR / Phase I
Award Amount:
$69,743.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Raul J Conti
Abstract:
N/a

ADVANCED AEROTHERMOCHEMISTRY ALGORITHM

Award Year / Program / Phase:
1991 / SBIR / Phase II
Award Amount:
$535,000.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Raul J Conti
Abstract:
A computer based algorithm is proposed that integrtes an advanced navier-stokes hypersonic flow solver with state-of-the-art material response computer codes to create a powerful tool for reentry vehicle heatshield design. complex gas physics are modeled with consideration of thermal and chemical… More

INNOVATIVE MODEL FOR REACTING FLOWS

Award Year / Program / Phase:
1991 / SBIR / Phase I
Award Amount:
$48,662.00
Agency:
NASA
Principal Investigator:
Abstract:
N/a

INNOVATIVE MODEL FOR REACTING FLOWS

Award Year / Program / Phase:
1992 / SBIR / Phase II
Award Amount:
$416,239.00
Agency:
NASA
Principal Investigator:
Abstract:
This project explores the benefits of a new computational model for reacting flows. it applies to non-equilibrium flows, in general, but is specially designed to address the frequent condition in hypersonic flows where some of the reactants are near thermochemical equilibrium, while the remainder… More

RF Performance Measurements in Simulated Reentry Environments

Award Year / Program / Phase:
1993 / SBIR / Phase I
Award Amount:
$72,789.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Raul J. Conti
Abstract:
N/a

Development of Base-Flow Computer Code

Award Year / Program / Phase:
1993 / SBIR / Phase I
Award Amount:
$63,000.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Raul J. Conti
Abstract:
N/a

Unitary Numerical Method For Flow And Heatshield Analysis

Award Year / Program / Phase:
1995 / SBIR / Phase I
Award Amount:
$69,904.00
Agency:
NASA
Principal Investigator:
Raul J. Conti , President
Abstract:
N/a

Coupling of Computational Fluid Dynamics (CFD), Reentry Vehicle Surface Ablations, and In-Depth Conductions

Award Year / Program / Phase:
2005 / SBIR / Phase I
Award Amount:
$98,993.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Raul J. Conti, President
Abstract:
The proposed innovation consists of developing a stand-alone computational tool to predict simultaneously the hypersonic flowfield and the thermal response of the heatshield of vehicles entering the atmosphere at high speed, including the full coupling of the fluid an solid phenomena involved. In… More

Coupling of Computational Fluid Dynamics (CFD), Reentry Vehicle Surface Ablations, and In-Depth Conductions

Award Year / Program / Phase:
2006 / SBIR / Phase II
Award Amount:
$748,533.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Raul J. Conti, President
Abstract:
The proposed innovation consists of developing and testing an integrated computational tool capable of predicting simultaneously the hypersonic flow over a reentry vehicle and the response of its thermal protection system, including surface ablation, recession, and in- depth thermal conduction, as… More