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  • Launch System Reuse

    Paper number

    IAC-18,D2,1,6,x43039

    Author

    Mr. Akhil Gujral, United States, The Aerospace Corporation

    Coauthor

    Dr. William Emanuelsen, United States, The Aerospace Corporation

    Coauthor

    Mr. Randolph Kendall, United States, The Aerospace Corporation

    Coauthor

    Dr. Walter Lauderdale, United States, United States Air Force

    Coauthor

    Mr. Jon Strizzi, United States, United States Air Force

    Year

    2018

    Abstract
    Launch vehicle providers are advancing technology for reusable launch systems and beginning to demonstrate them at an unprecedented pace. Reusable launch vehicles for orbital space launch has the potential to reduce the cost of space access in the commercial sector and for National Security Space (NSS) launches, but cost savings is not the only nor the most significant factor for the Air Force to consider. Reusable launch vehicles may also offer higher reliability, increased responsiveness, and greater flexibility than expendable systems. The U.S. Air Force Launch Enterprise is evaluating how to best leverage reusable launch vehicle technology while integrating it into the existing flight worthiness certification process.  NSS missions have a low tolerance for risk and require high reliability launchers. Existing Mission Assurance (MA) processes and standards (e.g., reliability, testing, parts) were developed for expendable, one-time use launch systems.  Expendable and reusable launch systems alike must undergo the Air Force’s rigorous design validation and as-built verifications.  However, reusable systems are subject to reentry environments and extended hardware life-cycles due to multiple launches, recoveries, refurbishments, and re-tests.  Inspection of previously flown vehicles may allow improvements to the design and operations for subsequent launches. Previously flown boosters may also support assured access to space by providing additional assets with reduced lead time.  Upper stages, support infrastructure, and payloads must also be designed to support rapid, responsive and flexible launch. Given that the existing and envisioned medium to heavy (Evolved Expendable Launch Vehicle - class) reusable launch systems are still in their relative infancy, it is not yet clear whether the potential benefits will be obtained. While adhering to established EELV tenets for mission success, the Air Force launch system reuse strategy is pursuing a forward-leaning approach of researching and understanding the challenges of reuse, gathering data, gaining insight from government and commercial launch system partners, augmenting mission assurance processes and standards as appropriate, and pursuing the use of demonstration missions. This paper will highlight some of the areas that the USAF and The Aerospace Corporation are beginning to explore, including updates to specifications and standards, Independent Verification & Validation (IV&V) tools, added inspections, reuse parts traceability, and more to establish the technical baseline from which the Air Force will make future flight worthiness determinations for launch. These efforts will help determine whether and how National Security Space launch can benefit from the development of reusable launch systems.
    Abstract document

    IAC-18,D2,1,6,x43039.brief.pdf

    Manuscript document

    IAC-18,D2,1,6,x43039.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.