Mechanical Interfaces Sample Clauses

Mechanical Interfaces. The Spacecraft shall be mated to the upper stage via a Saab Ericsson Space 1194VS adapter and separation system. The adapter and the SC shall be encapsulated in the payload fairing prior to mating with the Zenit-3SL. The SC to LV mechanical interfaces shall be compatible with the mechanical interfaces specified in the Sea Launch User’s Guide, Section 7.1 and the Inmarsat -4 IRD, reference document number 4
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Mechanical Interfaces. 3.2.1 Piping Interfaces *
Mechanical Interfaces. 10 2.3.2 Electrical Interfaces.................................................10 2.3.3 Spacecraft/spacecraft Adapter Interface Test Support..................11 2.4 Spacecraft Separation Conditions........................................11 2.5
Mechanical Interfaces. The Spacecraft shall be mated to the upper stage via a Sea Launch provided SCA702+ spacecraft adapter (SCA) and separation system. The adapter and the SC shall be encapsulated in the payload fairing prior to mating with the Zenit 3SL. The SC to LV mechanical interfaces shall be compatible with the mechanical interfaces specified in the Sea Launch User's Guide, section 7.1.
Mechanical Interfaces. The Spacecraft shall be mated to the upper stage via a Launch Provider provided spacecraft adapter (SCA) and Clampband Opening Device (CBOD) separation system. The adapter and the SC shall be encapsulated in the payload fairing prior to mating with the lower stages. The SC to LV mechanical interfaces shall be compatible with the mechanical interfaces specified in the Atlas Launch System Mission Planner’s Guide (ref. A-4). Mission unique configurations shall supersede the Atlas Launch System Mission Planner’s Guide (ref. A-4), and shall be specified in the SC to LV ICD.
Mechanical Interfaces. 3.1.1 Adapter interface Adapter Interface: 1194 The Payload Adapter System to be used for JUPITER mission is either PAS 1194VS or PAS 1194C as described in Annex 8 of the MUA 5. The clamp band tension will be defined in accordance with the spacecraft mass and centre of gravity height with respect to the separation plane. Part 1 – JUPITER
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Mechanical Interfaces 

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