Comparison of Propulsion Options for a Lunar Lander Ascent Stage
Year: 2005
Type: conference-paper
DOI: 10.2514/6.2005-6740
Author: Joshua Hopkins
Institution: Lockheed Martin (United States)
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W2162451005
