DocumentCode :
2435283
Title :
Transfer of Files Between the Deep Impact Spacecrafts and the Ground Data System Using CFDP: a Case Study
Author :
Sanders, Felicia A. ; Jones, Grailing, Jr. ; Levesque, Michael
Author_Institution :
Jet Propulsion Lab., Pasadena
fYear :
2007
fDate :
3-10 March 2007
Firstpage :
1
Lastpage :
5
Abstract :
The CCSDS File Delivery Protocol (CFDP) Standard could reshape ground support architectures by enabling applications to communicate over the space link using reliable-symmetric transport services. JPL utilized the CFDP standard to support the Deep Impact Mission. The architecture was based on layering the CFDP applications on top of the CCSDS Space Link Extension Services for data transport from the mission control centers to the ground stations. On July 4, 2005 at 1:52 A.M. EDT, the Deep Impact impactor successfully collided with Comet Tempel 1. During the final 48 hours prior to impact, over 300 files were uplinked to the spacecraft, while over 10 thousand files were downlinked from the spacecraft using the CFDP during the encounter timeframe. This paper uses the Deep Impact Mission as a case study in a discussion of the CFDP architecture, Deep Impact Mission requirements, and design for integrating the CFDP into the JPL deep space support services. Issues and recommendations for future missions using CFDP are also provided.
Keywords :
data communication; protocols; space communication links; CCSDS File Delivery Protocol Standard; CFDP Standard; Deep Impact Mission; deep impact spacecrafts; deep space support services; files transfer; ground data system; reliable-symmetric transport services; space link; Application software; Communication standards; Communication system software; Data systems; Laboratories; Propulsion; Protocols; Software testing; Space missions; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2007 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
1-4244-0524-6
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2007.352896
Filename :
4161373
Link To Document :
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