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LM Concept is Responsive & Affordable

LM Concept is Responsive & Affordable. Approved for Public Release, Distribution Unlimited. Driving Responsiveness Features. Surge and all weather capability (cat 2) Robust vehicle with performance margin Horizontal stage integration Vehicle self test and checkout

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LM Concept is Responsive & Affordable

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  1. LM Concept is Responsive & Affordable Approved for Public Release, Distribution Unlimited

  2. Driving Responsiveness Features Surge and all weather capability (cat 2) Robust vehicle with performance margin Horizontal stage integration Vehicle self test and checkout Stage integration & launch in <24 hours Preloaded inert fuel Fault-tolerant avionics Simple field operations: - Factory mated T- 0 disconnects - “OneClick” Vehicle/Payload field joint - Only 2 fluids loaded at the launch area - No pyrotechnics/no hydraulics Responsiveness SLV Responsiveness Features • System design driven by responsive operations requirements instead of typical performance driven requirements Hybrid Propulsion & Basing Flexibility are Key Elements For Responsive Space Anytime, Anywhere, Affordable Launch Approved for Public Release, Distribution Unlimited

  3. Video of LM Falcon/SLV Concept Approved for Public Release, Distribution Unlimited

  4. Falcon SLV Performance • SLV-DS meets all mission performance requirements • Single vehicle design accomplishes two different mission profiles • Small satellite delivery to orbit (100 nm x 100 nm from KSC): • 1,000 lb minimum • 1,855 lb maximum • Hypersonic test vehicle profile • 2,000 lb minimum • 3,055 lb maximum 10 Ft 28.6 Ft 72.7 Ft SLV-DS Achieves All Performance Requirements with a Single Vehicle Approved for Public Release, Distribution Unlimited

  5. Hybrid Propulsion Test Heritage • Unique SLV Uses hybrid propulsion • Low cost materials • Inert and non toxic fuel • Zero explosive potential • Basic rubber • Motors cast at NASA’s MAF • Stop/Start and throttle capability • Shutting flow of LO2 stops thrust • Eliminates range destruct pyrotechnics • Flight demonstrated hybrid propulsion in 2002 • Full-scale second-stagemotor tested at AFRL 60 Klbf Motor Flight Test 600+ Development Tests 250 Klbf Multi-Port Motor Firing Falcon Full-Scale 2nd Stage Motor Firing 16 Years of Continuous Hybrid Propulsion Experience Establish The Basis For SLV Approved for Public Release, Distribution Unlimited

  6. RR101 Motor Firing – January 2005 • First Test 4 Months after ATP • 60 Second Burn Time • 500 psi OBJECTIVES: • Acquire the critical data necessary to validate the analytical baseline for LMF900 multi-row, multi-port hybrid technology • Combustion stability • Regression rate • Thrust • Chamber pressures • Port to port pressures • Low frequency vibration • High frequency G levels • Demonstrate increased performance of LMF900 • Baseline residuals Successful Firing Increased Technology Readiness Level and Grounded Falcon SLV Sizing Parameters Approved for Public Release, Distribution Unlimited

  7. Approved for Public Release, Distribution Unlimited

  8. Multi-row Multi-port Fuel GrainPerformed As Predicted • RR101 Acquired critical data to validate the analytical baseline for multi-row, multi-port hybrid technology • Stable Combustion • Favorable Regression • Thrust within Predictions • Isp within Predictions Post-test Pre-Test RR101 Results Incorporated Into Vehicle Design & Next Test Article Approved for Public Release, Distribution Unlimited

  9. RR102 Motor Firing – May 2005 • Second Test Planned 4 Months after RR101 • 120 Second Burn Time • 900 psi OBJECTIVES: • Acquire the critical data necessary to refine the analytical baseline for LMF900 multi-row, multi-port hybrid technology • Combustion stability • Regression rate consistency • Thrust • Chamber pressures • Port to port pressures • Low frequency vibration • High frequency G levels • Residuals Consistency • Fuel Integrity • 75% Flight Duration AFRL Test Stand RR101 Shown – RR102 Similar RR102 Completes Falcon Phase IIa Testing Approved for Public Release, Distribution Unlimited

  10. Falcon SLV Summary • SLV system design driven by responsive operations requirements • FALCON SLV is a significant spiral in the development of operationally responsive space • Designed for operational speed and flexibility • Costs approaching $5M including operations & range costs • PDR in June 2005 • SLV full-scale flight in 2007 Innovative Hybrid SLV On-Track For 2007 Flight Demonstration Approved for Public Release, Distribution Unlimited

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