SBIR/STTR Research Award

Propulsion and Logistics Systems

Award identifier 4c9534752d708cf2cd737294840355efcb767ee91f3eeaecc20d5561e24aed35Awarding agency Department of Defense · Missile Defense Agency

Award amount

$64,054

Program and phase

SBIR · Phase I

Award year

2001

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Award details

Awarding agency
Department of Defense
Branch
Missile Defense Agency
Recipient company
MACH I Inc.
Proposal award date
Not reported
Contract end date
Not reported
UEI
E4XRRLCUQGB5
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Solid propellants with significantly higher density impulse vs conventional aluminumbased propellants can be prepared utilizing zirconium metal fuel. This has beenindependently demonstrated by several investigators including Atlantic Research Corp-oration, a commercial propellant manufacturer. The extreme electrostatic discharge(ESD) sensitivity of zirconium metal has prevented its use in high density impulsepropellants. In a previous SBIR from NSWC, MACH I demonstrated and developed surfacepassivation technologies to dramatically improve the ESD sensitivity of hafnium metalfor use in energetics.In preliminary internal R&D, MACH I has shown this technology to be feasible forzirconium metal, dramatically improving its ESD sensitivity from 0.00025 to a safelevel of 0.036 joules. Since this technology involves forming a surface intermetal-lic with aluminum, there should not be a significant impact on reactivity or densityimpulse. We are proposing a program to optimize the ESD sensitivity improvement,reactivity, and impulse of the zirconium propellants. Atlantic Research Inc. wouldbe a subcontractor to MACH I testing reactivity and other propellant properties. Onepound of the optimum material would be produced in Phase I. In phase II, this wouldbe further developed and propellants commercialized. Zr Energy, a domestic producerof zirconium has committed to supply materials to this program and could quickly com-mercially produce the passivated zirconium should the technology be successfullydeveloped.The proposed program has the potential to greatly improve the safety and handlingcharacteristics of zirconium metal thus making high density impulse zirconium propel-lants a reality. The 15% higher density impulse of these propellants vs conventionalaluminum based propellants gives the system designer the flexibility of eithersmaller lighter rocket motors for a given impulse and pay-load requirement or largerimpulse and payload capabilities for a given motor size.Dual use benefits to the civilian automotive and light truck industries would berealized by improving the safety and handling characteristics of zirconium metal.Zirconium potassium chlorate accidents cause two fatalities in 1998/9 due to ESDrelated problems.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

22 SBIR/STTR records share this UEI (1988–2016). Reported award amounts total $6,271,599. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Transportation

Agency intelligence

Department of Defense

Back to SBIR/STTR Research Awards

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