SBIR/STTR Research Award

Properties Investigation of High-MON Oxidizers and MMH Blends for Use in Deep Space Exploration

Award identifier 432299b03ce8fca265ecd565a1cfa551f49b9f61f05a616573d742998441f3acAwarding agency National Aeronautics and Space Administration

Award amount

$749,675

Program and phase

STTR · Phase II

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
FRONTIER AEROSPACE CORP
Proposal award date
2020-02-04
Contract end date
2022-02-03
UEI
CFTNLSS6BY36
Solicitation number
STTR_18_P2
Topic code
T9

Research abstract

The REFPROP program developed by the National Institute of Standards and Technology (NIST) is a widely-used database for industrial fluid properties, including propellants used for chemical rocket propulsion.nbsp; For deep space applications, low-temperature propellants are of particular interest but accurate fluid property data was scarce or unavailable to the industry.nbsp; Recently, NASA MSFC has funded several research programs (including this proposal#39;s phase I contract) to develop capabilities of handling and measuring the physical, thermodynamic, and system properties of Modified Oxides of Nitrogen (MON), which is Nitrogen Tetraoxide (NTO) blended with various percentages of Nitrous Oxide.nbsp; High-MON blends (15-30% NO) have a significantly lower freezing point than neat NTO and promise to enable cold-propellant operation in hypergolic rocket engines when paired with Monomethyl Hydrazine (MMH). The fluid property data resulting from these studies would best serve the engineering community if made available in the REFPROP program from the NIST and this proposal seeks to author the collected data into a freely-availablenbsp;library under NIST direction.nbsp;Additionally, although the freezing point of MMH approaches -60deg;C and it should be usable with MON down to -40deg;C, the viscosity of MMH increase rapidly below 0deg;C.nbsp;This may causenbsp;flow and mixing problems that can inhibit ignition and steady operation.nbsp; In a previous Department of Defense program, it was demonstrated that adding a compound to a similar fuel resulted innbsp;lower viscosity without negatively impacting combustion efficiency.nbsp; To characterize the results of blending MMH similarly, this proposal also seeks to investigatenbsp;key physical properties of MMH-blends at cold temperatures andnbsp;perform hypergolic ignition and hypergolic performance testing with MON-25.nbsp; Like the MON data, the results of these studies will be authored into the REFPROP libraries for general distribution.

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

2 SBIR/STTR records share this UEI (2018–2020). Reported award amounts total $870,158. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

Agencies: National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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