Accession Number : AD0474552


Title :   STANDARD SPACE LAUNCH VEHICLE TO SIMULATED LABORATORY.


Corporate Author : MARTIN CO DENVER COLO


Report Date : 15 Oct 1965


Pagination or Media Count : 15


Abstract : This Interface Specification (IFS) defines the structural, mechanical, electrical, and test capabilities and constraints which shall exist between the Titan III Standard Space Launch Vehicle (SSLV) and the Payload. This specification covers those areas of interface peculiar to the MOL-EFT Program at Titan III Station 77.0. This IFS shall be effective for the Standard Space Launch System (SSLS) utilizing the Integrate Transfer Launch (ITL) concept at ETR for SSLV No. 9 (Configuration C) and its Payload in their use on the MOL-EFT (HSQ Flight) Program. (Author)


Descriptors :   *MANNED SPACECRAFT , *LAUNCH VEHICLES , SPECIFICATIONS , PAYLOAD , LIQUID PROPELLANT ROCKET ENGINES , FLIGHT TESTING , MECHANICAL PROPERTIES , STRUCTURAL PROPERTIES , ELECTRICAL GROUNDING , FLIGHT CONTROL SYSTEMS


Subject Categories : Liquid Propellant Rocket Engines
      Ground Support Sys & Facil For Space Vehicles


Distribution Statement : APPROVED FOR PUBLIC RELEASE