Start Date

4-1981 8:00 AM

Description

Augmented performance is necessary to assure that the full Space Shuttle payload deployment capability of 32,000 Ibs can be achieved for the 98° inclination, 150 nautical mile circular mission launched from Vandenberg AFB, Calif. The performance-augmented Space Shuttle meets all design mission requirements, and offers potential payload growth to accommodate new payloads and new concepts. Consequently, it is important to the future national space capability that performance augmentation be developed and made available to meet payload requirements which exploit the capability of the Space Shuttle.

This paper presents the options under consideration which include uprating the Space Shuttle Main Engines (SSMEs) to the range of 115 percent of rated power level for nominal operations, Solid Rocket Motor (SRM) filamentwound case segments, and the Liquid Boost Module (LBM). These candidates will be studied in detail for the remainder of FY81 and FY82. Selection and initiation of development in FY83 will support the early 1987 need date.

Comments

No other information or file available for this session.

Share

COinS
 
Apr 1st, 8:00 AM

Planning for Performance Augmentation of Space Shuttle

Augmented performance is necessary to assure that the full Space Shuttle payload deployment capability of 32,000 Ibs can be achieved for the 98° inclination, 150 nautical mile circular mission launched from Vandenberg AFB, Calif. The performance-augmented Space Shuttle meets all design mission requirements, and offers potential payload growth to accommodate new payloads and new concepts. Consequently, it is important to the future national space capability that performance augmentation be developed and made available to meet payload requirements which exploit the capability of the Space Shuttle.

This paper presents the options under consideration which include uprating the Space Shuttle Main Engines (SSMEs) to the range of 115 percent of rated power level for nominal operations, Solid Rocket Motor (SRM) filamentwound case segments, and the Liquid Boost Module (LBM). These candidates will be studied in detail for the remainder of FY81 and FY82. Selection and initiation of development in FY83 will support the early 1987 need date.

 

To view the content in your browser, please download Adobe Reader or, alternately,
you may Download the file to your hard drive.

NOTE: The latest versions of Adobe Reader do not support viewing PDF files within Firefox on Mac OS and if you are using a modern (Intel) Mac, there is no official plugin for viewing PDF files within the browser window.