NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Concept of Operations for a Prospective "Proving Ground" in the Lunar VicinityNASA is studying a "Proving Ground" near the Moon to conduct human space exploration missions in preparation for future flights to Mars. This paper describes a concept of operations ("conops") for activities in the Proving Ground, focusing on the construction and use of a mobile Cislunar Transit Habitat capable of months-long excursions within and beyond the Earth-Moon system. Key elements in the conops include the Orion spacecraft (with mission kits for docking and other specialized operations) and the Space Launch System heavy-lift rocket. Potential additions include commercial launch vehicles and logistics carriers, solar electric propulsion stages to move elements between different orbits and eventually take them on excursions to deep space, a node module with multiple docking ports, habitation and life support blocks, and international robotic and piloted lunar landers. The landers might include reusable ascent modules which could remain docked to in-space elements between lunar sorties. The architecture will include infrastructure for launch preparation, communication, mission control, and range safety. The conops describes "case studies" of notional missions chosen to guide the design of the architecture and its elements. One such mission is the delivery of a ~10-ton pressurized element, co-manifested with an Orion on a Block 1B Space Launch System rocket, to the Proving Ground. With a large solar electric propulsion stage, the architecture could enable a year-long mission to land humans on a near-Earth asteroid. In the last case, after returning to near-lunar space, two of the asteroid explorers could join two crewmembers freshly arrived from Earth for a Moon landing, helping to safely quantify the risk of landing deconditioned crews on Mars. The conops also discusses aborts and contingency operations. Early return to Earth may be difficult, especially during later Proving Ground missions. While adding risk, limited-abort conditions provide needed practice for Mars, from which early return is likely to be impossible.
Document ID
20150019623
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Love, Stanley G.
(NASA Johnson Space Center Houston, TX, United States)
Hill, James J.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
October 22, 2015
Publication Date
March 5, 2016
Subject Category
Space Sciences (General)
Lunar And Planetary Science And Exploration
Report/Patent Number
JSC-CN-34540
Report Number: JSC-CN-34540
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available