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Title Laser rocket system analysis
Publication Date1982 Feb 01
OSTI IdentifierOSTI ID: 6595781
Report Number(s)N-82-18584
Resource TypeTechnical Report
Resource RelationOther Information: In NASA. Langley Research Center, Space Laser Power Transmission System Studies, p 123-134 (SEE N82-18578 09-36)
Research OrgLockheed Missiles and Space Co., Inc., Sunnyvale, CA (USA)
Subject14 SOLAR ENERGY; LASERS; USES; SPACE VEHICLES; CONTROL SYSTEMS; COST; MIRRORS; ORBITAL SOLAR POWER PLANTS; THRUSTERS; POWER PLANTS; SOLAR POWER PLANTS; VEHICLES
Description/AbstractPotential national space transportation budget savings offered by laser rocket systems are considered. Orbital payload transportation costs, requiring 16 MW laser power space based or 37.5 MW ground based, are reduced by a factor of 2.4. The SPS orbital transportation costs, requiring 490 MW laser power space based or 1000 MW ground based, are reduced by factors up to 7. Technology advancement is indicated for the laser, thruster, large lightweight adaptive mirror, and pointing and tracking.
Country of PublicationUnited States
LanguageEnglish
FormatMedium: X; Size: Pages: 22
AvailabilityNTIS, PC A10/MF A01.
System Entry Date2008 Feb 08

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