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Conceptual Launch Vehicle and Spacecraft Design for Risk AssessmentOne of the most challenging aspects of developing human space launch and exploration systems is minimizing and mitigating the many potential risk factors to ensure the safest possible design while also meeting the required cost, weight, and performance criteria. In order to accomplish this, effective risk analyses and trade studies are needed to identify key risk drivers, dependencies, and sensitivities as the design evolves. The Engineering Risk Assessment (ERA) team at NASA Ames Research Center (ARC) develops advanced risk analysis approaches, models, and tools to provide such meaningful risk and reliability data throughout vehicle development. The goal of the project presented in this memorandum is to design a generic launch 7 vehicle and spacecraft architecture that can be used to develop and demonstrate these new risk analysis techniques without relying on other proprietary or sensitive vehicle designs. To accomplish this, initial spacecraft and launch vehicle (LV) designs were established using historical sizing relationships for a mission delivering four crewmembers and equipment to the International Space Station (ISS). Mass-estimating relationships (MERs) were used to size the crew capsule and launch vehicle, and a combination of optimization techniques and iterative design processes were employed to determine a possible two-stage-to-orbit (TSTO) launch trajectory into a 350-kilometer orbit. Primary subsystems were also designed for the crewed capsule architecture, based on a 24-hour on-orbit mission with a 7-day contingency. Safety analysis was also performed to identify major risks to crew survivability and assess the system's overall reliability. These procedures and analyses validate that the architecture's basic design and performance are reasonable to be used for risk trade studies. While the vehicle designs presented are not intended to represent a viable architecture, they will provide a valuable initial platform for developing and demonstrating innovative risk assessment capabilities.
Document ID
20150000182
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Motiwala, Samira A.
(Stanford Univ. Stanford, CA, United States)
Mathias, Donovan L.
(NASA Ames Research Center Moffett Field, CA United States)
Mattenberger, Christopher J.
(Science and Technology Corp. Moffett Field, CA, United States)
Date Acquired
January 6, 2015
Publication Date
June 1, 2014
Subject Category
Launch Vehicles And Launch Operations
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2014-218366
ARC-E-DAA-TN15822
Funding Number(s)
CONTRACT_GRANT: NNX14AF94A
CONTRACT_GRANT: NNA10DF26C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Launch Vehicle
Spacecraft
Assessment
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