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Effects of extreme acceleration, microgravity, and deceleration on Bacillus subtilis onboard a suborbital space flight. [PDF]
Yang E +12 more
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3 months transit time to Mars for human missions using SpaceX Starship. [PDF]
Kingdon J.
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Free-flight and tracking experiments of a multi-parabola laser propulsion vehicle. [PDF]
Takahashi M +3 more
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On feasibility of launch vehicle designs
Applied Mathematics and Computation, 2005zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Angelo Miele, T. Wang, P. N. Williams
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Pre-Launch Diagnostics for Launch Vehicles
2008 IEEE Aerospace Conference, 2008This paper discusses the opportunities for automating pre-launch fault detection and diagnostics for launch vehicles, by using ground-based computers to analyze data obtained from the pre-launch umbilical during integrated test and launch countdown operations in near-real time. Automation will improve the time to diagnose and isolate failures, which is
Mark Schwabacher, Robert Waterman
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NASA Crew Launch Projects Overview: The Crew Launch Vehicle and The Cargo Launch Vehicle Systems
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006The U.S. Vision for Space Exploration (January 2004) serves as the foundation for the National Aeronautics and Space Administration's (NASA) strategic goals and objectives. As the NASA Administrator outlined during his confirmation hearing in April 2005, these include: 1) Flying the Space Shuttle as safely as possible until its retirement, not later ...
Jimmy Snoddy +2 more
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Semireusable Launch Vehicle: A Next-Generation Launch Vehicle?
Journal of Spacecraft and Rockets, 2001Advanced launch systems studies are ongoing at MAN Technologie AG, Karlsfeld, Germany, contributing to a broader European effort that is examining options for the next space transportation system to be developed there. One promising candidate that uses medium-term technologies is a vertical takeoff semireusable launch vehicle featuring a reusable ...
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SAE Technical Paper Series, 1984
<div class="htmlview paragraph">Vehicles capable of lifting very large and heavy payloads into low earth orbit (LEO) will be needed to support certain large-scale space missions being considered for the late 1990-2000 time period. These missions include the support of strategic national commitments, large space power systems, and interplanetary ...
William R. Marshall +2 more
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<div class="htmlview paragraph">Vehicles capable of lifting very large and heavy payloads into low earth orbit (LEO) will be needed to support certain large-scale space missions being considered for the late 1990-2000 time period. These missions include the support of strategic national commitments, large space power systems, and interplanetary ...
William R. Marshall +2 more
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AMROC Industrial Launch Vehicle: A Low Cost Launch Vehicle
SAE Technical Paper Series, 1987<div class="htmlview paragraph">American Rocket Company is engaged in design and development of an expendable launch vehicle to be used for placing moderate size payloads in low Earth orbit. The primary drivers in the design are reliability and low cost.
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Risk assessment of satellite launch with reusable launch vehicle
Reliability Engineering & System Safety, 2001Abstract A new methodology is developed for assessing the risk associated with launching satellites in space by use of Reusable Launch Vehicles (RLVs). The objective is to assess the Maximum Probable Loss (MPL) for third party insurance purposes, which is a requirement for licensing of private operators. Launch industry convention has been to execute
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