2005
DOI: 10.7249/mg276
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Lessons Learned from the F/A-22 and F/A-18 E/F Development Programs

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Cited by 13 publications
(5 citation statements)
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“…Previous studies have looked at the environment factors that impact the effectiveness of EVMS application. These include project controls experience (Wolf 2014), project management ability (Weaver 2016), culture (King 2018), communication (McNamee andImmonen 2019;Turner and Müller 2004), EVM technical knowledge (Kim 2000), effective decision making (Bolinger and Phillips 2018;Younossi et al 2005), accurate and timely data (Shi 2019;Hunter et al 2014), technology tools (Weaver 2016), and lack of engagement (Kim 2000), among many others. In the EVMS knowledge area, some specific EVMS environment factors have been investigated; however, there is a need for a comprehensive EVMS environment factor compilation made up of key factors around which an assessment method can be designed.…”
Section: Evms Environmentmentioning
confidence: 99%
“…Previous studies have looked at the environment factors that impact the effectiveness of EVMS application. These include project controls experience (Wolf 2014), project management ability (Weaver 2016), culture (King 2018), communication (McNamee andImmonen 2019;Turner and Müller 2004), EVM technical knowledge (Kim 2000), effective decision making (Bolinger and Phillips 2018;Younossi et al 2005), accurate and timely data (Shi 2019;Hunter et al 2014), technology tools (Weaver 2016), and lack of engagement (Kim 2000), among many others. In the EVMS knowledge area, some specific EVMS environment factors have been investigated; however, there is a need for a comprehensive EVMS environment factor compilation made up of key factors around which an assessment method can be designed.…”
Section: Evms Environmentmentioning
confidence: 99%
“…Providing performance guarantees of the structure, the main criteria for the box design must be assured. Mechanical properties of the carbon fiber composite, such as, high tensile and compressive elastic modulus, high notched tensile and notched compressive strength of the carbon fiber composite, offershigh flaperon efficiency, sufficient buckling stability of skins and spar webs, as well as, high bearing strength for load introductions [28,29]. Figure 3 shows a typical of the structure of the front fuselage in the cockpit area and it demonstrates how here too the same criteria as for the wing are mainly valid.…”
Section: Introductionmentioning
confidence: 94%
“…The airframe and avionics experienced 42 and 25 percent cost growth from 1996 to 2002, respectively. 45 The program also experienced schedule delays of up to a year for delivery of airframes due to airframe manufacturing difficulties. 46 Although technology alone is not responsible for cost and schedule overruns, evidence of immature technology contributing to program risk exists.…”
Section: Risk Managementmentioning
confidence: 99%