IN SPACE, L.L.C.

Address

3495 KENT AVE STE G100
WEST LAFAYETTE, IN, 47906-1334

http://www.inspacellc.com

Information

DUNS: 132073946
# of Employees: 9

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. Vapor Containment and Fire Suppression System for Hypergolic Propellants

    Amount: $999,647.00

    Toxicity and fire risks associated with monomethylhydrazine and nitrogen tetroxide must be mitigated for the continued fielding of divert and attitude control systems for MDA interceptors. In a Phase ...

    SBIRPhase II2011Department of Defense Missile Defense Agency
  2. Design Tools for Combustion Stability

    Amount: $996,027.00

    ABSTRACT: A joint experimental and computational project using a carefully designed, flexible test article is proposed to assess the velocity-coupled combustion response of a representative liquid ro ...

    SBIRPhase II2011Department of Defense Air Force
  3. 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 ...

    STTRPhase II2009Missile Defense Agency Department of Defense
  4. Vapor Containment and Fire Suppression System for Hypergolic Propellants

    Amount: $92,485.00

    Hydrazine-based fuels and nitrogen tetroxide-based oxidizers have been the propellants of choice for many propulsion systems over the last several decades due to the propellant combination’s high sp ...

    SBIRPhase I2009Missile Defense Agency Department of Defense
  5. Design Tools for Combustion Stability

    Amount: $98,475.00

    The combination of complex physics and extremely severe combustor environments presents a formidable challenge to engineers who must ensure that high-pressure, high-performance rocket engines are stab ...

    SBIRPhase I2009Air Force Department of Defense
  6. 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 ...

    SBIRPhase I2008Department of Defense Air Force
  7. 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 ...

    STTRPhase II2008Air Force Department 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 ...

    SBIRPhase I2007National Aeronautics and Space Administration
  9. 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 ...

    STTRPhase I2006Missile Defense Agency Department of Defense
  10. 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 ...

    STTRPhase I2006Air Force Department of Defense

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