Primary Intelligence Asset
A Trans-Atmospheric Turbojet Engine
Declassified Public record OCR verified
INTEL
Executive Summary
This document outlines a DARPA SBIR Phase I award granted to Hmx, Inc. for developing a trans-atmospheric turbojet propulsion system. The proposed engine integrates a conventional turbojet core with liquid oxidizer injection to achieve continuous operation from takeoff to orbit in turbojet, rocket, or combined modes. Potential applications include orbital space transport, high-speed point-to-point delivery, and military strike/reconnaissance aircraft.
Analysis Confidence: High
ST_CODE: 54031
System Metadata
Source ID
DOC-54031
Process Date
Public archive record
Integrity Hash
SHA256-54031...
Indexer Status
COMPLETE
Source Document (Web Archive)
This document was archived from a web source. No PDF version is available.
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Transcript
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Award Information
Award Title: A Trans-Atmospheric Turbojet Engine
Awardee: Hmx, Inc.
Address: 350 South Center Street, Reno, NV, 89501 0950 USA
Award Year: 2001
UEI: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Congressional District: N/A
Program: SBIR Phase I
Awarding Agency: DOD / DARPA
Total Award Amount: $97,763
Contract Number: DAAH0102CR071
Agency Tracking Number: 01SB2-0163
Solicitation Year: 2001
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This document outlines a DARPA SBIR Phase I award granted to Hmx, Inc. for developing a trans-atmospheric turbojet propulsion system. The proposed engine integrates a conventional turbojet core with liquid oxidizer injection to achieve continuous operation from takeoff to orbit in turbojet, rocket, ...