EARTH-TO-ORBIT RAILGUN LAUNCHER

被引：3

作者：

BROWN, JL ^{[1
]}

JAMISON, KA ^{[1
]}

JOHNSON, NE ^{[1
]}

ROLADER, GE ^{[1
]}

SCANLON, JJ ^{[1
]}

COUTEE, PW ^{[1
]}

机构：

[1] USAF,WRIGHT LAB ARMAMENT DIRECTORATE,EGLIN AFB,FL 32542

来源：

IEEE TRANSACTIONS ON MAGNETICS | 1993年 / 29卷 / 01期

关键词：

D O I：

10.1109/20.195603

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper provides an overview of a comprehensive study which examined the feasibility of launching relatively small payloads into orbit using electromagnetic launcher technology. The specific question addressed by the study was ''Should serious consideration be given to hypervelocity gun launch to space as an alternative to conventional rocket powered launch vehicles and, if so, why?'' An overview of the concept developed is provided along with discussion of the major subsystems.

引用

页码：373 / 378

页数：6

共 6 条

[1] RAILGUN PERFORMANCE WITH A 2-STAGE LIGHT-GAS GUN INJECTOR [J].

HAWKE, RS ;

SUSOEFF, AR ;

ASAY, JR ;

ANG, JA ;

HALL, CA ;

KONRAD, CH ;

WELLMAN, GW ;

HICKMAN, RJ ;

HEATH, WA ;

MARTINEZ, JR ;

SAUVE, JL ;

VASEY, AR ;

SHAHINPOOR, M .

IEEE TRANSACTIONS ON MAGNETICS, 1991, 27 (01) :28-32

[2]

LEE NW, 1991, HYPERVELOCITY LAUNCH

[3]

PALMER M, 1991, IEEE T MAG, V25, P393

[4]

PALMER M, 1989, ELECTROMAGNETIC SPAC

[5]

RICE EE, 1982, FINAL TECHNICAL REPO

[6]

ROLANDER GE, 1992, 6TH EML S AUST

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