Accession Number:

ADA361613

Title:

East Coast Abort Modeling with RTLS Elimination for the Space Shuttle-Liquid Fly Back Booster Launch System

Descriptive Note:

Master's thesis

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSONAFB OH

Personal Author(s):

Report Date:

1999-03-01

Pagination or Media Count:

184.0

Abstract:

This study investigates the ability of the proposed Liquid Fly Back Booster, a replacement for the Space Shuttles Solid Rocket Boosters SRBs, to eliminate the need for the Return to Launch Site RTLS abort mode. A Fortran model of a nominal launch trajectory was perturbed to simulate a single Space Shuttle Main Engine-out SSME-out abort scenario at different times in the launch with the goal being to abort to the southern most landing site possible. The model accounts for vehicle lift, drag, dynamic pressure, throttling times and includes atmospheric effects to enhance fidelity. Results show the RTLS abort mode can be eliminated and successful landings made as far south as Savannah, Georgia. This success is attributed to the throttling capability of the Liquid Fly Back Booster engines.

Subject Categories:

  • Manned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE