DocumentCode :
44250
Title :
Electromagnetic Augmentation Can Reduce Space Launch Costs
Author :
McNab, Ian R.
Author_Institution :
Inst. for Adv. Technol., Univ. of Texas at Austin, Austin, TX, USA
Volume :
41
Issue :
5
fYear :
2013
fDate :
May-13
Firstpage :
1047
Lastpage :
1054
Abstract :
A study was undertaken to determine if a ground-based electromagnetic (EM) acceleration system could provide a useful reduction in launch-to-orbit costs compared with current large chemical boosters, while increasing launch safety and reliability. The study evaluated EM augmentation of the chemical boost capability for a two-stage-to-low-Earth-orbit system, with the extreme case being a complete EM launch. Several EM acceleration options are available, but railguns were chosen for this study. The second stage of the system was assumed to be a chemical rocket or a reusable scramjet to carry a reusable orbiter vehicle into low-Earth orbit. EM launch systems of this type will be governed by the same fundamental principles as tactical guns, but one major difference will be that the EM accelerator track, which may be several kilometers in length, will not be powered only from the “breech” as in a tactical gun, since electrical resistive losses will be unacceptably large. To overcome this, a distributed feed system will be required. This study shows that the capital cost of the pulsed-power system for the EM accelerator will dominate the system economics. Present pulsed-power approaches will require many launches to offset the capital cost. Novel pulsed-power concepts or low-cost manufacturing approaches will need to be developed for such a concept to be economically attractive.
Keywords :
Earth orbit; aircraft power systems; electromagnetic launchers; jet engines; pulsed power supplies; rocket engines; space vehicles; EM accelerator track; EM augmentation evaluation; EM launch system; chemical boost capability; chemical rocket; distributed feed system; electrical resistive loss; ground-based electromagnetic acceleration system; launch reliability; launch safety; pulsed power system; reusable orbiter vehicle; reusable scramjet; space launch cost reduction; system economics; tactical gun; two-stage-to-low-Earth orbit system; Acceleration; Chemicals; Fuels; Orbits; Payloads; Rockets; Space vehicles; Economics; electromagnetic (EM) launch; pulsed power; space launch;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/TPS.2013.2241452
Filename :
6450106
Link To Document :
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