DocumentCode
358561
Title
K-1 integrated vehicle health management system: design for operational efficiency
Author
Bailey, Richard ; McSharry, Michael
Author_Institution
Kistler Aerosp. Corp., Kirkland, WA, USA
Volume
4
fYear
2000
fDate
2000
Firstpage
323
Abstract
Kistler Aerospace Corporation is developing the world´s first commercial, fully reusable aerospace vehicle. The two-stage K-1 vehicle is designed to significantly reduce the cost of reliably delivering payloads to Low Earth Orbit (LEO) and to provide rapid launch response and schedule flexibility. The K-1 operability philosophy is similar to that of late-generation commercial aircraft, such as the Boeing 777. The vehicle´s on-board systems are continually monitored for performance versus expected and this performance data is used for both in-flight and maintenance turn-around actions. The in-flight decisions are made, without a person-in-the-loop, to maximize the mission success. The operations crew on the ground obtains early visibility on the performance during the flight so they are prepared to perform the necessary actions to prepare the K-1 for the next flight. This paper discusses the avionics architecture, which is implemented with both managed and committed hardware redundancies. The managed redundancy exists in the triplex computing complexes and the committed redundancy exists in the dual pyrotechnic, valve, and motor effectors. The paper will discuss the avionics design and the implementation of the vehicle health management system
Keywords
aerospace instrumentation; avionics; computerised instrumentation; computerised monitoring; maintenance engineering; redundancy; K-1 integrated vehicle; K-1 operability philosophy; Kistler Aerospace Corporation; LEO; Low Earth Orbit; avionics architecture; avionics design; commercial aircraft; cost; flexibility; health management; maintenance turn-around; managed redundancy; mission success; operational efficiency; rapid launch response; reusable aerospace vehicle; two-stage K-1 vehicle; vehicle health management; Aerospace electronics; Aircraft; Computer architecture; Costs; Low earth orbit satellites; Monitoring; Payloads; Redundancy; Scheduling; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
0-7803-5846-5
Type
conf
DOI
10.1109/AERO.2000.878443
Filename
878443
Link To Document