Gb. Bruening et al., The potential impact of utilizing advanced engine technology for a combat capable unmanned air vehicle (UAV), J ENG GAS T, 123(3), 2001, pp. 508-512
Categorie Soggetti
Mechanical Engineering
Journal title
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME
This paper evaluates the potential impact of utilizing advanced engine tech
nology for a limited life, combat capable, unmanned air vehicle (UAV) appli
cation. A study was conducted to define payoffs in terms of mission capabil
ity and system level life cycle costs (LCC) associated with implementing th
ree different engine development approaches into a combat capable UAV desig
n. The three different approaches considered were: a new, advanced technolo
gy engine; an existing (off-the-shelf) engine; and a derivative of an exist
ing engine with limited technology insertion. A detailed vehicle configurat
ion design was developed to conduct this assessment, including a low observ
able (LO), highly integrated engine/airframe layout for survivability: and
mission adaptable considerations. The vehicle is designed with multirole mi
ssion capability such as suppression of enemy air defense (SEAD), close air
support (CAS), and battlefield air interdiction (BAI). A system level perf
ormance comparison is assessed with the three different engine approaches s
pecifically for the SEAD-type mission. For the cost analysis, the multirole
mission capability is reflected in the overall assumptions such as in the
number of aircraft needed to meet the mission requirements. A system level
assessment such as in this study is essential in determining,whether the ad
ditional costs associated with the development of a new, advanced engine is
worth the investment. The results of this study suggest that advanced engi
ne technology insertion cart provide significant benefits in terms of missi
on I range capability vehicle weight/size, and overall life cycle costs ver
sus an existing engine.