IPSEC configuration Clause Samples

The IPSEC configuration clause defines the requirements and parameters for establishing secure, encrypted communications between parties using IP Security (IPSEC) protocols. Typically, this clause outlines the specific technical standards, authentication methods, and encryption algorithms that must be used, and may specify responsibilities for configuring and maintaining the IPSEC tunnels. Its core practical function is to ensure that data transmitted over networks remains confidential and protected from unauthorized access, thereby addressing security and compliance concerns in data exchange.
IPSEC configuration. C.3.1 IP interconnect will require the use of IPsec, SRTP or TLS for the security of underlying layers C.3.2 The following guidelines are to be followed for IPsec implementation: • Tunnel mode only is supported for IPsec. Transparent mode is not supported. • 4 types of transform sets are supported: ‘esp-3des-md5’, ‘esp-3des-sha1’, ‘esp- aes128-md5’, ‘esp-aes128-sha1’. ‘esp-3des-md5’ is the preferred transform set. • ‘Main Mode’ is the only method supported for IKE negotiation. ‘Aggressive Mode’ is not supported. • Perfect Forward Secrecy (PFS) shall be used in ‘group 2’.
IPSEC configuration. C.3.1 IP interconnect will require the use of IPsec, SRTP or TLS for the security of underlying layers C.3.2 The following guidelines are to be followed for IPsec implementation: • Tunnel mode only is supported for IPsec. Transparent mode is not supported. • 4‘etsypp‐aeesso1f2t8r‐amnsdf5o’r,m‘essept‐saaerse12su8p‐sphoar1te’.d‘:e‘seps‐p3‐d3edse‐sm‐md5d’5i’s, ‘thesepp‐3redfeesr‐rsehdat1r’a,nsform set. • ‘Main Mode’ is the only method supported for ▇▇▇ negotiation. ‘Aggressive Mode’ is not supported. • Perfect Forward Secrecy (PFS) shall be used in ‘group 2’.

Related to IPSEC configuration

  • Configuration The configuration for the Purchase Right Aircraft will be the Detail Specification for Model 767-3S2F aircraft at the revision level in effect at the time of the Supplemental Agreement. Such Detail Specification will be revised to include (i) changes required to obtain required regulatory certificates and (ii) other changes as mutually agreed upon by Boeing and Customer.

  • AIRCRAFT CONFIGURATION The guarantees defined below ("the Guarantees") are applicable to the A330-200 Aircraft as described in the Technical Specification ***, as amended by the Specification Change Notices ("SCN's") for:

  • Functionality Customer is entitled to additional functionality previously purchased or bundled with the software if available in the version or update released on or after the start date of the Agreement. Customer acknowledges that certain functionality in current and previous software versions may not be available in future upgrades. Added functionality may require additional paid services (clinical and technical) to configure and support.

  • Architecture The Private Improvements shall have architectural features, detailing, and design elements in accordance with the Project Schematic Drawings. All accessory screening walls or fences, if necessary, shall use similar primary material, color, and detailing as on the Private Improvements.

  • Configuration Management The Contractor shall maintain a configuration management program, which shall provide for the administrative and functional systems necessary for configuration identification, control, status accounting and reporting, to ensure configuration identity with the UCEU and associated cables produced by the Contractor. The Contractor shall maintain a Contractor approved Configuration Management Plan that complies with ANSI/EIA-649 2011. Notwithstanding ANSI/EIA-649 2011, the Contractor’s configuration management program shall comply with the VLS Configuration Management Plans, TL130-AD-PLN-010-VLS, and shall comply with the following: