A Brief Description of Fit Check Exercises for Space Vehicle (Single or Multiple) Integration onto a Launch Vehicle

Abstract

Based on previous experiences of (single and multiple) space vehicle (SV) integration onto the launch vehicle (LV) throughout the Space Test Program (STP) mission history, it was noted that a dry run (or fit check) of the installation/integration exercise was invaluable as a precursor to a successful launch integration activity. This paper is written to introduce and assist any payload and/or launch provider in the fit check objectives, specific sequential (time-based) activities with descriptions and desired outcomes for each step. A flow chart accompanies the write-up to further illustrate the inclusion and insertion of these events within the program integrated master schedule (IMS) during the launch activity flow.

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Document Details

Document Type
Technical Report
Publication Date
Aug 30, 2019
Accession Number
AD1114578

Entities

People

  • Arthur A. Menichiello
  • Peter S. Chang

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Acquisition
  • Adapters
  • Air Force
  • Center Of Gravity
  • Computer Simulations
  • Computer-Aided Design
  • Computers
  • Defense Systems
  • Dispensers
  • Ground Support
  • Ground Support Equipment
  • Launch Vehicles
  • Lessons Learned
  • Mass
  • Missions
  • Moment Of Inertia
  • National Security
  • Security
  • Simulators
  • Solar Panels
  • Spacecraft
  • United States
  • Vehicles

Readers

  • Aerospace Engineering.
  • Computer Science.
  • Systems Analysis and Design

Technology Areas

  • Space