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Evolution and Impact of Saturn V on Space Launch System from a Guidance, Navigation, and Mission Analysis PerspectiveThe Saturn V launch vehicle represented a jump in capability for heavy lift launch vehicles, enabling the Lunar Orbit Rendezvous approach to planetary exploration employed by the Apollo program 50 years ago. Following Apollo, and the development of the Space Transportation System, the NASA space exploration program shifted focus from lunar exploration to long-term, sustained, re-usable access to Low Earth Orbit. With the recent focus of NASA on the Artemis program and continued exploration of cislunar space as a precursor to Martian exploration, the shift has swung back to heavy lift capability. To meet this need, NASA has developed the Space Launch System. While the vehicle is a new design, it is heavily influenced by the engineering solutions and approach used on the Saturn V while taking advantage of the state of the art of launch vehicle design. The approach to abort, for example, shares many familiarities with the triggers and concept of operations used on Saturn V. Analysis approaches to dispersed trajectory performance are also very similar, but advances in computing technology have enabled a much more expanded set of inputs that can be modelled and assessed in a rapid manner. Additionally, guided flight algorithms share similar first principles but have expanded to include day of launch wind information. Trajectory optimization has also advanced significantly due to the availability of computing resources, but similar maneuvers and profiles are flown across both vehicles. Also, while the approach of onboard inertial navigation has been maintained between the two programs, the shift from platform to strapdown systems enables reduced complexity in the system design while maintaining required performance. As described, the Space Launch System is the evolution of NASA launch vehicle designs, owing a large heritage to the Saturn vehicle program and incorporating advances in propulsion systems, avionics, computing, and sensor technology over the past 50 years.


Document ID
20190033307
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Ahmad, Naeem
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Anzalone, Evan J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Craig, A. Scott
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Dukeman, Gregory A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
December 1, 2019
Publication Date
October 21, 2019
Subject Category
Space Transportation And Safety
Report/Patent Number
IAC-19, D2,9-D6.2,6,x52986
M19-7661
Report Number: IAC-19, D2,9-D6.2,6,x52986
Report Number: M19-7661
Meeting Information
Meeting: International Astronautical Congress (IAC)
Location: Washington, DC
Country: United States
Start Date: October 21, 2019
End Date: October 25, 2019
Sponsors: International Astronautical Federation (IAF-HQ)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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