Applications: Other
Pages 174–186 (13 pages)
Text on page 183
Space Applications SpaceX Starship rocket is expected to continue to reduce cost to orbit and enable larger battery applications to support expanded mission capacity. APPLICATIONS
AMBIENT PRESSURE
MISSION EXAMPLE
CELL CHEMISTRY EXAMPLE
AVG. MISSION DURATION
RADIATION
AVG. TEMPERATURE
DESIGN CHALLENGES
EARTH
101.3 kPa
Electric vehicle
Graphite + NCM
812 years
H3, Be-7, C14,Na-22 0.21mSv/year
30°C to 40°C
Corrosion
UPPER ATMOSPHERE
200 Pa
Stratostats
Graphite + LCO
100 days
He, Li- through Fe ions Neutrons 110 MeV 1.2 Neutrons/cm^2/s,
20°C to 60°C
Low temperatures, icing, pressure variations
LOW EARTH ORBIT LEO
106 - 109 Pa
ISP satellites
Graphite + NCA or LFP
30 days (humans) 4 26 years (constellations)
100010 M Protons and Electrons/cm2/s
65°C to 125°C
Sealing under frequent temperature variation
GEOSYNCHRONOUS ORBIT GEO
1012 Pa
Media broadcasting
Graphite + NCA or Nickel Hydrogen
7 years (many operating past EOL
400500 km/s Protons & Electrons 30/cm^2/s
196°C to 128°C
Calendar life, high cycle-life
LUNAR
3 109 Pa
Lunar rover
Pu-238 RTG (radioisotope thermal generator)
3 months design, 31 months life Jade Rabbit rover)
Protons, Electrons 1010000 MeV, 110 Protons/cm2/s
130°C to 120°C
Extended duration of hot and cold/dark periods
MARS
560 Pa
Martian rover
Graphite + NCA
90 days NASA design Opportunity lasted 15 years)
Protons, Electrons 11000 MeV, 1001000/s
153°C to 20°C
Sealing under temperature variation, RTG radiation
DEEP SPACE
1014 - 1018 Pa
Deep space probes
Pu-238 RTG (radioisotope thermal generator)
45+ years Voyager)
Protons, Electrons 110,000 MeV 10010,000/s
Calendar life, RTG radiation and decreasing heating
Source: 1 NASA 2 Virtue Market Research 3 E3S 4 Zhang, J., et al. 5 ESA 6 Singh, L., et al. 7 NASA 8 IDA Org 9 Naito, M., et al. 10 Guo, J., et al. 11 NASA 12 Phys Org 13 NASA 14 NASA 15 Space Flight
Extracted from the PDF; charts and images may read imperfectly.
Page 183 · 10/13