Railgun space launcher
Document Type
Article
Publication Date
10-1-2010
Abstract
A method and facilities for delivering payload and people into outer space are presented. This method uses, in general, engines located on a planetary surface. The installation consists of a space apparatus, power drive stations, which include a fly-wheel accumulator (for storage) of energy, a variable reducer, a powerful homopolar electric generator, and electric rails. The drive stations accelerate the apparatus up to hypersonic speed. The estimations and computations show the possibility of making this project a reality in a short period of time (for payloads that can tolerate high g forces). The launch will be very cheap at a projected cost of $3-$5/lb. The authors developed a theory of this type of the launcher. © 2010 ASCE.
Identifier
77956825101 (Scopus)
Publication Title
Journal of Aerospace Engineering
External Full Text Location
https://doi.org/10.1061/(ASCE)AS.1943-5525.0000041
ISSN
08931321
First Page
293
Last Page
299
Issue
4
Volume
23
Recommended Citation
Bolonkin, Alexander and Krinker, Mark, "Railgun space launcher" (2010). Faculty Publications. 6057.
https://digitalcommons.njit.edu/fac_pubs/6057
