Many items of aircraft equipment are capable of being repaired when they fail. Whether or not these items should be repaired or discarded upon failure is a complex problem that has important implications for design, life cycle cost, and operational requirements. Treating any of these factors separately can lead to seriously suboptimal results. A procedure is presented here that offers a unified approach to repair-discard decisions. The procedure addresses design, cost, and operational requirements, and it is compatible with the logistic support analysis (LSA) process as called out in MIL-STD-1388 (Reference 2).
Repair-discard concepts in design
Entwurf eines Reparatur-Ausschuss-Konzeptes
1982
4 Seiten, 4 Bilder, 4 Quellen
Conference paper
English
INSTANDHALTUNG , ORGANISATIONSPLAN , REPARATUR , ERSATZTEIL , KUNDENDIENST , ENTSCHEIDUNGSBAUM , KOSTEN , LEBENSDAUER , FLUGZEUG , BETRIEBSSICHERHEIT , TOLERANZ , RECHNERUNTERSTUETZUNG , KOMPATIBILITAET , FEHLERWAHRSCHEINLICHKEIT , AUSFALL , SCHADEN , STOERUNG , ZUVERLAESSIGKEIT , FEHLERANALYSE , WIRTSCHAFTLICHKEIT
Projectile/sabot discard aerodynamics
AIAA | 1980
|Aerodynamic Interference during Sabot Discard
AIAA | 1978
|Aerodynamic interference during sabot discard
AIAA | 1977
|Aerodynamics of asymmetric sabot discard
AIAA | 1982
|Aerodynamics of asymmetric sabot discard
AIAA | 1983
|