IN Space, L.L.C.

Company Information

Company Name
IN Space, L.L.C.
Address
3495 Kent Avenue
Suite G100
West Lafayette, IN, -
Phone
1 765-775-2107
URL
http://www.inspacellc.com
DUNS
132073946
Number of Employees
9

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$474,057.00
5
SBIR Phase II
$1,745,980.00
2
STTR Phase I
$268,217.00
4
STTR Phase II
$1,295,314.00
3
Chart code to be here

Award List

  1. Thermal Decomposer for Peroxide

    Amount: $69,896.00

    Thermal decomposition of hydrogen peroxide may provide significant weight, operability, envelope, and cost benefits over traditional catalytic decomposition units used in propulsion and energy systems ...

    STTR Phase I 2003 Missile Defense AgencyDepartment of Defense
  2. Hypergolic Swirl Injectors for Advanced Divert and Attitude Control Systems

    Amount: $86,489.00

    The majority of liquid bipropellant engines in the United States employ impinging jet injectors. While they offer moderately high combustion efficiency and are design from an extensive knowledgebase, ...

    SBIR Phase I 2004 Missile Defense AgencyDepartment of Defense
  3. Lightweight Liquid Target Booster Thrust Chamber Assembly

    Amount: $479,572.00

    MDA is interested in the development of hydrogen peroxide/hydrocarbon engines for liquid target vehicles. A large reduction in engine weight (~75%) and technical risk are possible by eliminating the ...

    STTR Phase II 2004 Missile Defense AgencyDepartment of Defense
  4. Lightweight Liquid Target Booster Thrust Chamber Assembly

    Amount: $0.00

    MDA is interested in the development of hydrogen peroxide/hydrocarbon engines for liquid target vehicles. A large reduction in engine weight (~75%) and technical risk are possible by eliminating the ...

    STTR Phase I 2004 Missile Defense AgencyDepartment of Defense
  5. Novel Binder Materials for IM-compliant Solid Rocket Motors

    Amount: $98,480.00

    The need for munitions insensitive to stimuli possible to occur in the logistical and operational life cycle of the munition is paramount for safeguarding life and property. Research to produce IM-co ...

    STTR Phase I 2006 Missile Defense AgencyDepartment of Defense
  6. Combustion Stability Innovations for Liquid Rocket Engines

    Amount: $99,841.00

    While guidelines for stable combustion in certain engine cycles and propellant combinations exist; there is no proven, mechanistic predictive model, particularly for high-performance liquid hydrocarbo ...

    STTR Phase I 2006 Air ForceDepartment of Defense
  7. Variable Thrust, Multiple Start Hybrid Motor Solutions for Missile and Space Applications

    Amount: $99,190.00

    Energy management in missile systems can provide substantial performance advantages, especially for modern missiles capable of all-aspect engagements. Maximum flexibility is offered by a system that ...

    SBIR Phase I 2008 Office of the Secretary of DefenseDepartment of Defense
  8. Innovative Swirl Injector for LOX and Hydrocarbon Propellants

    Amount: $97,418.00

    Gases trapped in the propellant feed lines of space-based rocket engines due to cryogenic propellant boil-off or pressurant ingestion can result in poor combustion efficiencies, combustion instabiliti ...

    SBIR Phase I 2007 National Aeronautics and Space Administration
  9. Modeling and Simulation of the Stability of ORSC Main Combustion Chambers

    Amount: $499,933.00

    The potential for combustion instability has historically been a hindrance in developing rocket engines, and nearly always represents the major technical risk in engine developments. This proposal add ...

    STTR Phase II 2008 Air ForceDepartment of Defense
  10. Novel Binder Materials for IM-compliant Solid Rocket Motors

    Amount: $315,809.00

    The need for munitions insensitive to unplanned stimuli possible in the logistical and operational life cycle of a munition is paramount for safeguarding life and property. To help meet this need, IN ...

    STTR Phase II 2009 Missile Defense AgencyDepartment of Defense

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