TY - GEN
T1 - Propelling interplanetary spacecraft utilizing water-steam
AU - Martinez, Jorge
AU - Thangavelautham, Jekan
N1 - Publisher Copyright:
© 2019, Univelt Inc. All rights reserved.
PY - 2019
Y1 - 2019
N2 - Beyond space exploration, there are plans afoot to identify pathways to enable a space economy, where human live and work in space. One critical question is what are the resources required to sustain a space economy? Water has been identified as a critical resource both to sustain human-life but also for use in propulsion, attitude-control, power, thermal and radiation protection systems. Water may be obtained off-world through In-Situ Resource Utilization (ISRU) in the course of human or robotic space exploration that replace materials that would otherwise be shipped from Earth.” Water has been highlighted by many in the space community as a credible solution for affordable/sustainable exploration. Water can be extracted from the Moon, C-class Near Earth Objects (NEOs), surface of Mars and Martian Moons Phobos and Deimos and from the surface of icy, rugged terrains of Ocean Worlds. However, use of water for propulsion faces some important technological barriers. A technique to use water as a propellant is to electrolyze it into hydrogen and oxygen that is then pulsedetonated. High-efficiency electrolysis requires use of platinum-catalyst based fuel cells. Even trace elements of sulfur and carbon monoxide found on planetary bodies can poison these cells making them unusable. In this work, we develop steam-based propulsion that avoids the technological barriers of electrolyzing impure water as propellant. Using a solar concentrator, heat is used to extract the water which is then condensed as a liquid and stored. Steam is then formed using the solar thermal reflectors to concentrate the light into a nanoparticle- water mix. This solar thermal heating (STH) process converts 80 to 99% of the incoming light into heat. In theory, water can be heated to 1000 K to 3000K with a resulting Isp from 190s to 320s. This propulsion system can offer higher thrust than current electrical propulsion methods and represents a high delta-v solution for small spacecrafts. A further understanding of the concentration system, implications for GNC and the heat transfer process in the nanofluid is presented in this work.
AB - Beyond space exploration, there are plans afoot to identify pathways to enable a space economy, where human live and work in space. One critical question is what are the resources required to sustain a space economy? Water has been identified as a critical resource both to sustain human-life but also for use in propulsion, attitude-control, power, thermal and radiation protection systems. Water may be obtained off-world through In-Situ Resource Utilization (ISRU) in the course of human or robotic space exploration that replace materials that would otherwise be shipped from Earth.” Water has been highlighted by many in the space community as a credible solution for affordable/sustainable exploration. Water can be extracted from the Moon, C-class Near Earth Objects (NEOs), surface of Mars and Martian Moons Phobos and Deimos and from the surface of icy, rugged terrains of Ocean Worlds. However, use of water for propulsion faces some important technological barriers. A technique to use water as a propellant is to electrolyze it into hydrogen and oxygen that is then pulsedetonated. High-efficiency electrolysis requires use of platinum-catalyst based fuel cells. Even trace elements of sulfur and carbon monoxide found on planetary bodies can poison these cells making them unusable. In this work, we develop steam-based propulsion that avoids the technological barriers of electrolyzing impure water as propellant. Using a solar concentrator, heat is used to extract the water which is then condensed as a liquid and stored. Steam is then formed using the solar thermal reflectors to concentrate the light into a nanoparticle- water mix. This solar thermal heating (STH) process converts 80 to 99% of the incoming light into heat. In theory, water can be heated to 1000 K to 3000K with a resulting Isp from 190s to 320s. This propulsion system can offer higher thrust than current electrical propulsion methods and represents a high delta-v solution for small spacecrafts. A further understanding of the concentration system, implications for GNC and the heat transfer process in the nanofluid is presented in this work.
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M3 - Conference contribution
AN - SCOPUS:85079486902
SN - 9780877036616
T3 - Advances in the Astronautical Sciences
SP - 499
EP - 510
BT - Guidance, Navigation, and Control, 2019
A2 - Hallowell, Heidi E.
PB - Univelt Inc.
T2 - 42nd AAS Rocky Mountain Section Guidance and Control Conference, 2019
Y2 - 31 January 2019 through 6 February 2019
ER -