F-22 ECS/TMS Qualification Test Program Overview

972261

07/01/1997

Event
International Conference On Environmental Systems
Authors Abstract
Content
Qualification Testing is performed to verify that component and system designs will operate successfully in their intended environment. The F-22 ECS/TMS is currently well into its component and system qualification testing. With 143 components varying widely in function and complexity, substantial experience has been gained in both design knowledge as well as understanding the value of the test process itself. This paper will address a summary of the test program efforts to date, focusing on lessons learned generally applicable to any product development effort. Specific areas to be discussed include:
  1. 1.
    An overview of the system functions and components.
  2. 2.
    A summary of the qualification test program goals and structure at component and system level.
  3. 3.
    Discussion of the basic test environments required.
  4. 4.
    Importance of a good closed loop failure reporting and corrective action system (FRACAS).
  5. 5.
    Key elements of an effective test program.
  6. 6.
    Summary of test failures experienced to date, with corresponding corrective actions/lessons learned.
  7. 7.
    Overview of system and flight qualification tests yet to be performed.
Meta TagsDetails
DOI
https://doi.org/10.4271/972261
Pages
8
Citation
Sprouse, J., "F-22 ECS/TMS Qualification Test Program Overview," SAE Technical Paper 972261, 1997, https://doi.org/10.4271/972261.
Additional Details
Publisher
Published
Jul 1, 1997
Product Code
972261
Content Type
Technical Paper
Language
English