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Titre du document / Document title

Safety & design considerations for the cooperative avionics test bed (CATBird) aircraft

Auteur(s) / Author(s)

DELEHANT Edward J. (1) ;

Affiliation(s) du ou des auteurs / Author(s) Affiliation(s)

(1) Lockheed Martin Aeronautics

Résumé / Abstract

Lockheed Martin Aeronautics is currently in the process of modifying a 737-300 aircraft from the standard airline configuration to an avionics test bed aircraft for use in developing the Joint Strike Fighter (JSF) F-35 avionics suite. As simple of a concept as this implies, it is actually a complex design evolution as there are no recognized "standards" for test bed aircraft. The design evolution attempts to provide a recognized level of safety to an aircraft flown under an experimental airworthiness certificate. A test bed that most closely replicates the test article will be more productive. And, a test bed capable of testing all the desired systems both on an individual basis and as an integrated system will pay large returns to the test program.

Revue / Journal Title

SAE transactions    ISSN  0096-736X 

Source / Source

2005, vol. 114, no 1 (1580 p.)  [Document : 8 p.] (bibl.: dissem.), pp. 938-945 [8 page(s) (article)]

Langue / Language

Anglais

Editeur / Publisher

Society of Automotive Engineers, New York, NY, ETATS-UNIS  (1927-200) (Revue)

Mots-clés anglais / English Keywords

Experimental study

;

Test standard

;

Standard test

;

Program proof

;

Fight aircraft

;

Aeronautics

;

Avionics

;

Program verification

;

Aircraft

;

Safety

;

Mots-clés français / French Keywords

Etude expérimentale

;

Norme essai

;

Essai normalisé

;

Preuve programme

;

Avion combat

;

Aéronautique

;

Avionique

;

Vérification programme

;

Aéronef

;

Sécurité

;

Mots-clés espagnols / Spanish Keywords

Estudio experimental

;

Norma ensayo

;

Ensayo normalizado

;

Prueba programa

;

Avión combate

;

Aeronáutica

;

Aviónica

;

Verificación programa

;

Aeronave

;

Seguridad

;

Localisation / Location

INIST-CNRS, Cote INIST : 5876, 35400013318523.0900

Nº notice refdoc (ud4) : 17554600



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