Reconnection Electromagnetic Launcher (RCEML) and its Application

Shukang Cheng; Xiaopeng Li; Liyi Li; Hanying Gao; Yusheng Hu

Reconnection Electromagnetic Launcher (RCEML) and its Application

Shukang Cheng^*
, Xiaopeng Li
, Liyi Li
, Hanying Gao
, Yusheng Hu

^*Corresponding author for this work

School of Electrical Engineering and Automation

Harbin Institute of Technology

Research output: Contribution to journal › Conference article › peer-review

1 Scopus citations

Abstract

RCEML is a special electromagnetic device. In this paper, the equation of motion of the RCEML is presented. Speed characteristic of RCEML and autostability of projectile have been studied. A 1000-stage RCEML device is designed and simulated for small satellite on the basis of the research for the single-stage RCEML. The parametric evaluations of the RCEML have been concluded with a launcher length of 250m - 260m, tunnel at 5° inclination, last velocity of 8km/s, at which speed small satellite will achieve final orbit. The RCEML is suit for any application of small payload. Such as: planetary probes, nuclear waste launch, intercontinental ballistic artillery and so on.

Original language	English
Pages (from-to)	1672-1676
Number of pages	5
Journal	Conference Record - IAS Annual Meeting (IEEE Industry Applications Society)
Volume	3
State	Published - 2003
Event	2003 IEEE Industry Applications Conference; 38th Annual Meeting: Crossroads To Innovation - Salt Lake City, UT, United States Duration: 12 Oct 2003 → 16 Oct 2003

Keywords

High pulse magnetic
RCEML
Space application

Cite this

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title = "Reconnection Electromagnetic Launcher (RCEML) and its Application",

abstract = "RCEML is a special electromagnetic device. In this paper, the equation of motion of the RCEML is presented. Speed characteristic of RCEML and autostability of projectile have been studied. A 1000-stage RCEML device is designed and simulated for small satellite on the basis of the research for the single-stage RCEML. The parametric evaluations of the RCEML have been concluded with a launcher length of 250m - 260m, tunnel at 5° inclination, last velocity of 8km/s, at which speed small satellite will achieve final orbit. The RCEML is suit for any application of small payload. Such as: planetary probes, nuclear waste launch, intercontinental ballistic artillery and so on.",

keywords = "High pulse magnetic, RCEML, Space application",

author = "Shukang Cheng and Xiaopeng Li and Liyi Li and Hanying Gao and Yusheng Hu",

year = "2003",

language = "英语",

volume = "3",

pages = "1672--1676",

journal = "Conference Record - IAS Annual Meeting (IEEE Industry Applications Society)",

issn = "0197-2618",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

note = "2003 IEEE Industry Applications Conference; 38th Annual Meeting: Crossroads To Innovation ; Conference date: 12-10-2003 Through 16-10-2003",

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TY - JOUR

T1 - Reconnection Electromagnetic Launcher (RCEML) and its Application

AU - Cheng, Shukang

AU - Li, Xiaopeng

AU - Li, Liyi

AU - Gao, Hanying

AU - Hu, Yusheng

PY - 2003

Y1 - 2003

N2 - RCEML is a special electromagnetic device. In this paper, the equation of motion of the RCEML is presented. Speed characteristic of RCEML and autostability of projectile have been studied. A 1000-stage RCEML device is designed and simulated for small satellite on the basis of the research for the single-stage RCEML. The parametric evaluations of the RCEML have been concluded with a launcher length of 250m - 260m, tunnel at 5° inclination, last velocity of 8km/s, at which speed small satellite will achieve final orbit. The RCEML is suit for any application of small payload. Such as: planetary probes, nuclear waste launch, intercontinental ballistic artillery and so on.

AB - RCEML is a special electromagnetic device. In this paper, the equation of motion of the RCEML is presented. Speed characteristic of RCEML and autostability of projectile have been studied. A 1000-stage RCEML device is designed and simulated for small satellite on the basis of the research for the single-stage RCEML. The parametric evaluations of the RCEML have been concluded with a launcher length of 250m - 260m, tunnel at 5° inclination, last velocity of 8km/s, at which speed small satellite will achieve final orbit. The RCEML is suit for any application of small payload. Such as: planetary probes, nuclear waste launch, intercontinental ballistic artillery and so on.

KW - High pulse magnetic

KW - RCEML

KW - Space application

UR - https://www.scopus.com/pages/publications/0242592418

M3 - 会议文章

AN - SCOPUS:0242592418

SN - 0197-2618

VL - 3

SP - 1672

EP - 1676

JO - Conference Record - IAS Annual Meeting (IEEE Industry Applications Society)

JF - Conference Record - IAS Annual Meeting (IEEE Industry Applications Society)

T2 - 2003 IEEE Industry Applications Conference; 38th Annual Meeting: Crossroads To Innovation

Y2 - 12 October 2003 through 16 October 2003

ER -

Reconnection Electromagnetic Launcher (RCEML) and its Application

Abstract

Keywords

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