DocumentCode :
711230
Title :
Ensuring Cassini´s end-of-mission propellant margins
Author :
Sturm, Erick J. ; Barber, Todd J. ; Roth, Duane
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2015
fDate :
7-14 March 2015
Firstpage :
1
Lastpage :
9
Abstract :
The Cassini spacecraft is in its final years. On September 15, 2017, Cassini will plunge deep into Saturn´s atmosphere never to reemerge; thus concluding its second extended mission and 13 years in orbit around the ringed planet. As of October 2014, the spacecraft is four years in to its seven-year, second extended mission, the Cassini Solstice Mission (CSM). With three years left and only 2.5% of its loaded bipropellant and 37% of its loaded monopropellant remaining, the Cassini project actively manages the predicted end-of-mission propellant margins to maintain a high confidence in the spacecraft´s ability to complete the CSM as designed. Accurate spacecraft navigation, rigorous remaining-propellant estimation, and frequent future propellant consumption prediction have resulted in efficient propellant use and a probability of sufficient propellant margin greater than 99%.
Keywords :
Saturn; planetary atmospheres; probability; propellants; space vehicles; CSM; Cassini Solstice Mission; Cassini end-of-mission propellant margins; Cassini project; Cassini spacecraft; Saturn atmosphere; loaded monopropellant; probability; remaining-propellant estimation; second extended mission; spacecraft navigation; Fuels; Navigation; Orbits; Propulsion; Space vehicles; Trajectory; Uncertainty;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2015 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5379-0
Type :
conf
DOI :
10.1109/AERO.2015.7119015
Filename :
7119015
Link To Document :
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