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The cryptographic module design requirements of Flight Termination System for secure cryptogram delivery  

Hwang, Soosul (한국항공우주연구원 한국형발사체개발사업본부 발사체기술개발단 발사체전자팀)
Kim, Myunghwan (한국항공우주연구원 한국형발사체개발사업본부 발사체기술개발단 발사체전자팀)
Jung, Haeseung (한국항공우주연구원 한국형발사체개발사업본부 발사체기술개발단 발사체전자팀)
Oh, Changyul (한국항공우주연구원 한국형발사체개발사업본부 발사체기술개발단 발사체전자팀)
Ma, Keunsu (한국항공우주연구원 한국형발사체개발사업본부 발사체기술개발단 발사체전자팀)
Publication Information
Journal of Satellite, Information and Communications / v.10, no.3, 2015 , pp. 114-120 More about this Journal
Abstract
In this paper, we show the design requirements of the cryptographic module and its security algorithm designed to prevent the exposure of the command signal applied to Flight Termination System. The cryptographic module consists of two separate devices that are Command Insertion Device and Command Generation Device. The cryptographic module designed to meet the 3 principles(Confidentiality, Integrity and Availability) for the information security. AES-256 block encryption algorithm and SHA-256 Hash function were applied to the encrypted symmetric key encryption method. The proposed cryptographic module is expected to contribute to the security and reliability of the Flight Termination System for Space Launch Vehicle.
Keywords
Cryptographic Module; Security; Encryption; Decryption; Symmetric Key; Reliability;
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  • Reference
1 한국인터넷진흥원(KISA) 홈페이지, "암호이용활성화/암호소개," http://seed.kisa.or.kr/iwt/ko/index.do
2 황수설, 고정환, 이재득, "해외발사체 사례조사를 통한 FTS 명령방식 변천사 연구," 제11회 우주발사체기술 심포지움, pp. 283-289, 2010.
3 USC Title 44, Chapter 35, $\S$3542
4 한국인터넷진흥원(KISA), "암호이용 안내서," 2010.01
5 박영호, "공개키 암호,"물리학과 첨단기술, pp. 7-12, 2007.
6 한국인터넷진흥원(KISA), "암호이용활성화, 암호 키 관리 안내서," 2014.12
7 한국인터넷진흥원(KISA), "암호이용활성화, 암호기술 구현 안내서," 2013.12