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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Full Transcript

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, ...