Mechanical Interfaces Clause Samples

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
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.
Mechanical Interfaces. Piping Interfaces *
Mechanical Interfaces. Confidential information has been omitted and filed separately with the Securities and Exchange Commission pursuant to a request for Confidential Treatment.
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. 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. 3.1.1 Adapter interface
Mechanical Interfaces