NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
MSFC Advanced Concepts Office and the Iterative Launch Vehicle Concept MethodThis slide presentation reviews the work of the Advanced Concepts Office (ACO) at Marshall Space Flight Center (MSFC) with particular emphasis on the method used to model launch vehicles using INTegrated ROcket Sizing (INTROS), a modeling system that assists in establishing the launch concept design, and stage sizing, and facilitates the integration of exterior analytic efforts, vehicle architecture studies, and technology and system trades and parameter sensitivities.
Document ID
20110010230
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Creech, Dennis
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
February 25, 2011
Subject Category
Launch Vehicles And Launch Operations
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available