48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2012
DOI: 10.2514/6.2012-4152
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A Systems Approach to Developing an Affordable Space Ground Transportation Architecture using a Commonality Approach

Abstract: With better than 20 years' experience, the von Braun team preached and practiced that rocketand launch pad must be mated on the drawing board, if they were to be compatible at the launching. The new rocket went hand in hand with its launching facility. Moonport (NASA SP-4204) C. D. Benson & W. B. Faherty 1978This paper presents a structured approach for achieving a compatible Ground Systt:m (GS) and Flight System (FS) architecture that is affordable, productive and sustainable. This paper is an extension of th… Show more

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Cited by 6 publications
(4 citation statements)
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“…24 Similarly, the community needs to know where specific operations and support functions can be reduced by design of the flight system and through greater attention to investments in this area than are normally given during the marketing and initial design of a launch vehicle, for instance. 25,26,27,28,29 …”
Section: What Is Needed?mentioning
confidence: 99%
“…24 Similarly, the community needs to know where specific operations and support functions can be reduced by design of the flight system and through greater attention to investments in this area than are normally given during the marketing and initial design of a launch vehicle, for instance. 25,26,27,28,29 …”
Section: What Is Needed?mentioning
confidence: 99%
“…A paradigm shift in our design focus is needed 8 for space transportation to become more economical. This is an area SPST has been working for many years ( Ref 1,3,4,5, 8,9). Once this transportation cost is reduced significantly, the return on investment will become more attractive to these investors.…”
Section: What Are the Incentivesmentioning
confidence: 99%
“…Multiple propellants 5. Hypergolic propellants (safety) 6 The operations concerns that have been identified provided a basis for carefully examining the elements of the propulsion system that need to be addressed.…”
Section: Launch Vehicle Requirementsmentioning
confidence: 99%