NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Laser thrusterLaser propulsion can reduce fuel by 57 t to 105 t over chemical propulsion for a 144 t Lunar base, with no significant increase in trip time. Laser propulsion reduces trip time by a factor of 40 to 120 over nuclear electric propulsion and time in radiation belts by a factor of 100 to 1700. Either solar or nuclear driven laser diode arrays could produce multimegawatt beams, typically 3,700 t for a 235 MW laser system. Laser diode arrays have high payoff due to short wavelength (850 nm) and high diode efficiency (70 percent). A dry laser OTV of 8790 kg and 60 percent efficiency can transport a 144 t lunar base. Laser propulsion could carry both personnel and cargo safely to the lunar base.
Document ID
19900000848
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jalufka, N. W.
(Hampton Inst. VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1989
Publication Information
Publication: NASA. Langley Research Center, Second Beamed Space-Power Workshop
Subject Category
Lasers And Masers
Accession Number
90N10164
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available