N6426724C0051
Definitive Contract
Overview
Government Description
873AUTHORITY
Awardee
Awarding Agency
Funding Agency
Place of Performance
Mooresville, NC 28117 United States
Pricing
Cost Plus Fixed Fee
Set Aside
Small Business Set Aside - Total (SBA)
Extent Competed
Full And Open Competition After Exclusion Of Sources
Est. Average FTE
3
Related Opportunity
None
Corvid Technologies was awarded
Definitive Contract N6426724C0051 (N64267-24-C-0051)
for 873Authority
worth up to $1,199,998
by Naval Strategic Systems Programs
in July 2024.
The contract
has a duration of 2 years 2 months and
was awarded
through SBIR Topic Development of an Aerothermal Modeling and Simulation Code for Hypersonic Applications
with a Small Business Total set aside
with
NAICS 541715 and
PSC AC12
via direct negotiation acquisition procedures with 2 bids received.
As of today, the Definitive Contract has a total reported backlog of $299,998.
SBIR Details
Research Type
Small Business Innovation Research Program (SBIR) Phase II
Title
Development of an Aerothermal Modeling and Simulation Code for Hypersonic Applications
Related Solicitation
Abstract
Corvid and Leidos are partnering to create HAVOC (Hypersonic Aerothermostructural Vehicle-Oriented Coupling), an automated computational tool designed to analyze vehicle TPS (Thermal Protection Systems) through hypersonic trajectories. HAVOC employs high fidelity CFD (Computational Fluid Dynamics) and Finite Element Analysis (FEA) solvers to capture the complex physics that define hypersonic flight and a vehicle s response throughout a trajectory. Aerodynamic heating at high speeds results in surface thermochemistry as well as material temperature rise, leading to reduce material strength and thermal expansion, and nonlinear material responses to thermal and aerodynamic loads. Vehicle shape change then impacts aerodynamics and aeroheating, creating a need for a coupled workflow for analyzing hypersonic vehicle TPS.HAVOC builds upon the state-of-the-art workflow of using film coefficient and recovery state to define aeroheating boundary conditions for a transient thermal model of a hypersonic trajectory to include automatically updated CFD and FEA grids that respond to the changing shape of the vehicle. The result is a hands-off high fidelity tool that can predict TPS response to hypersonic flight in a fraction of the time and man-hour cost of previous tools.
Research Objective
The goal of phase II is to continue the R&D efforts initiated in Phase I. Funding is based on the results achieved in Phase I and the scientific and technical merit and commercial potential of the project proposed in Phase II.
Topic Code
N221-081
Agency Tracking Number
N2-8694
Solicitation Number
22.1
Contact
Greg Ryan
Status
(Open)
Last Modified 2/10/25
Period of Performance
7/10/24
Start Date
1/12/26
Current End Date
9/14/26
Potential End Date
Obligations and Backlog
$900.0K
Total Obligated
$900.0K
Current Award
$1.2M
Potential Award
$0.0
Funded Backlog
$300.0K
Total Backlog
Award Hierarchy
Definitive Contract
N6426724C0051
Subcontracts
Activity Timeline
Transaction History
Modifications to N6426724C0051
People
Suggested agency contacts for N6426724C0051
Competition
Number of Bidders
2
Solicitation Procedures
Negotiated Proposal/Quote
Evaluated Preference
None
Commercial Item Acquisition
Commercial Item Procedures Not Used
Simplified Procedures for Commercial Items
No
Other Categorizations
Subcontracting Plan
Plan Not Required
Cost Accounting Standards
Exempt
Business Size Determination
Small Business
Defense Program
None
DoD Claimant Code
None
IT Commercial Item Category
Not Applicable
Awardee UEI
DD7KTEMDG6A5
Awardee CAGE
1VJF8
Agency Detail
Awarding Office
N64267 NAVAL SURFACE WARFARE CENTER
Funding Office
N00030
Created By
christopher.mokbel@navy.mil
Last Modified By
christopher.mokbel@navy.mil
Approved By
christopher.mokbel@navy.mil
Legislative
Legislative Mandates
None Applicable
Performance District
NC-10
Senators
Thom Tillis
Ted Budd
Ted Budd
Representative
Patrick McHenry
Modified: 2/10/25