100%
Skip to main content
Platform
GovTribe AI
AI-powered insights to accelerate your government contracting workflow.
MCP Server
Connect GovTribe to your AI tools.
Beacon
Find and connect with key government decision-makers.
Profiles
Federal Agencies
Federal Contract Vehicles
Federal Grant Programs
Major Defense Acquisition Programs
NAICS Categories
PSC Categories
States
Jurisdictions
NIGP Categories
UNSPSC Categories
Vendors
Enrichment By Clearbit
Reports
New Entrants
Funding Analysis
Vehicle Analysis
Groups
Capture
Pipelines
Pursuits
Alerts
Teaming
Data
Awards
Forecasts
Federal Opportunities
State & Local Opportunities
Files
Prime and Subcontractors
Activity
Search
Exports
Solutions
Use Case
Opportunity Identification
Capture Management
Competitive Intelligence
Teaming & Partner Identification
Proposal Management
Strategic Leadership
Go-to-Market Strategy
Industry
Federal Contractors
State & Local Contractors
Grant Seekers
Government Agencies
Research & Consulting
Pricing
More
About Us
Features
Get A Demo
Sign Up
Blog
User Guide
Data Model
GovTribe for Agents
Login
Contact sales
Try for free
Login
Contact sales
Try for free
All Federal Grant Awards
Cooperative Agreement NNX08AD14A
Award Date
12/15/07
Completion Date
1/13/11
Dollars Obligated
$750K
Overview
Activity
9
Transactions
18
Subawards
Similar Awards
Federal Agency
National Aeronautics and Space Administration
Awardee
Congressional District Programs, Inc. (FFEHTGBH6GS9)
Federal Grant Program
43.001
Assistance Type
Cooperative Agreement
Place of Performance
Falls Church, VA 22044, USA
Update #1
Update #2
DEMONSTRATION OF A 3000 DEGREE COMPOSITE STRUCTURE TPSTHE PRIMARY OBJECTIVE OF THIS PROJECT IS TO DE
Posted 12/31/07
5
1
2
3
4
Mod #
Description
ReasonForModification
Federal Obligation
Date
8
DEMONSTRATION OF A 3000 DEGREE COMPOSITE STRUCTURE TPS THE PRIMARY OBJECTIVE OF THIS PROJECT IS TO DEMONSTRATE A LOAD BEARING THERMAL PROTECTION SYSTEM THAT IS LIGHTWEIGHT, RELIABLE, AND REUSABLE. A HONEYCOMB MATERIAL HAS BEEN MADE FROM CERAMIC PAPER, AND TESTS HAVE SHOWN THAT ITS COMPRESSIVE STRENGTH IS SUITABLE FOR USE AS A LOAD BEARING TPS. CELLS OF THE SAME HONEY COMB MATERIAL WERE FILLED WITH INSULATION, AND TESTS SHOWED THAT IT FUNCTIONED WELL AS A THERMAL PROTECTION SYSTEM. THE RESEARCH TEAM PROPOSES TO OPTIMIZE THIS DESIGN FOR USE IN HYPERSONIC VEHICLES. THE TEAM WILL MEASURE THE BASIC PROPERTIES OF THE CERAMIC PAPER SO THAT THE HONEYCOMB STRUCTURE CAN BE OPTIMIZED USING FINITE ELEMENT ANALYSIS. HONEYCOMB SAMPLES WILL BE ASSEMBLED AND TESTED TO VERIFY THE MODEL. THE TEAM WILL INVESTIGATE MATERIALS, COATINGS AND BONDING METHODS APPROPRIATE TO MATCH THE FACE SHEET MATERIAL WITH THE COMPOSITE HONEYCOMB STRUCTURE. THIS DESIGN IS EXPECTED TO ELIMINATE COMPLEX ATTACHMENT SCHEMES. PRELIMINARY DATA INDICATES THE PANELS WILL BE MORE RELIABLE AND LIGHTER IN WEIGHT THAN AETB, IF USED IN A COMPARABLE APPLICATION.
Funding Only Action
$0
9/8/11
Not listed
DEMONSTRATION OF A 3000 DEGREE COMPOSITE STRUCTURE TPSTHE PRIMARY OBJECTIVE OF THIS PROJECT IS TO DEMONSTRATE A LOAD BEARING THERMAL PROTECTION SYST
$0
9/8/11
7
DEMONSTRATION OF A 3000 DEGREE COMPOSITE STRUCTURE TPS THE PRIMARY OBJECTIVE OF THIS PROJECT IS TO DEMONSTRATE A LOAD BEARING THERMAL PROTECTION SYSTEM THAT IS LIGHTWEIGHT, RELIABLE, AND REUSABLE. A HONEYCOMB MATERIAL HAS BEEN MADE FROM CERAMIC PAPER, AND TESTS HAVE SHOWN THAT ITS COMPRESSIVE STRENGTH IS SUITABLE FOR USE AS A LOAD BEARING TPS. CELLS OF THE SAME HONEY COMB MATERIAL WERE FILLED WITH INSULATION, AND TESTS SHOWED THAT IT FUNCTIONED WELL AS A THERMAL PROTECTION SYSTEM. THE RESEARCH TEAM PROPOSES TO OPTIMIZE THIS DESIGN FOR USE IN HYPERSONIC VEHICLES. THE TEAM WILL MEASURE THE BASIC PROPERTIES OF THE CERAMIC PAPER SO THAT THE HONEYCOMB STRUCTURE CAN BE OPTIMIZED USING FINITE ELEMENT ANALYSIS. HONEYCOMB SAMPLES WILL BE ASSEMBLED AND TESTED TO VERIFY THE MODEL. THE TEAM WILL INVESTIGATE MATERIALS, COATINGS AND BONDING METHODS APPROPRIATE TO MATCH THE FACE SHEET MATERIAL WITH THE COMPOSITE HONEYCOMB STRUCTURE. THIS DESIGN IS EXPECTED TO ELIMINATE COMPLEX ATTACHMENT SCHEMES. PRELIMINARY DATA INDICATES THE PANELS WILL BE MORE RELIABLE AND LIGHTER IN WEIGHT THAN AETB, IF USED IN A COMPARABLE APPLICATION.
Funding Only Action
$0
7/25/11
Not listed
DEMONSTRATION OF A 3000 DEGREE COMPOSITE STRUCTURE TPSTHE PRIMARY OBJECTIVE OF THIS PROJECT IS TO DEMONSTRATE A LOAD BEARING THERMAL PROTECTION SYST
$0
7/25/11
6
THE PRIMARY OBJECTIVE OF THIS PROJECT IS TO DEMONSTRATE A LOAD BEARING THERMAL PROTECTION SYSTEM THAT IS LIGHTWEIGHT, RELIABLE, AND REUSABLE. A HONEYCOMB MATERIAL HAS BEEN MADE FROM CERAMIC PAPER, AND TESTS HAVE SHOWN THAT ITS COMPRESSIVE STRENGTH IS SUITABLE FOR USE AS A LOAD BEARING TPS. CELLS OF THE SAME HONEY COMB MATERIAL WERE FILLED WITH INSULATION, AND TESTS SHOWED THAT IT FUNCTIONED WELL AS A THERMAL PROTECTION SYSTEM. THE RESEARCH TEAM PROPOSES TO OPTIMIZE THIS DESIGN FOR USE IN HYPERSONIC VEHICLES. THE TEAM WILL MEASURE THE BASIC PROPERTIES OF THE CERAMIC PAPER SO THAT THE HONEYCOMB STRUCTURE CAN BE OPTIMIZED USING FINITE ELEMENT ANALYSIS. HONEYCOMB SAMPLES WILL BE ASSEMBLED AND TESTED TO VERIFY THE MODEL. THE TEAM WILL INVESTIGATE MATERIALS, COATINGS AND BONDING METHODS APPROPRIATE TO MATCH THE FACE SHEET MATERIAL WITH THE COMPOSITE HONEYCOMB STRUCTURE. THIS DESIGN IS EXPECTED TO ELIMINATE COMPLEX ATTACHMENT SCHEMES. PRELIMINARY DATA INDICATES THE PANELS WILL BE MORE RELIABLE AND LIGHTER IN WEIGHT THAN AETB, IF USED IN A COMPARABLE APPLICATION.
Funding Only Action
$58.4k
12/8/10