Mathematics – Logic
Scientific paper
Jan 2002
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002aipc..608..345m&link_type=abstract
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM- STAIF 2002. Conference on Thermophyiscs in Microgravity; Conference on In
Mathematics
Logic
Spaceborne And Space Research Instruments, Apparatus, And Components, Servo And Control Equipment, Robots, Industrial And Technological Research And Development
Scientific paper
Parachutes used for Mars landing missions are only certified for deployment at Mars behind blunt bodies flying at low angles of attack, Mach numbers up to 2.2, and dynamic pressures of up to 800 Pa. NASA is currently studying entry vehicle concepts for future robotic missions to Mars that would require parachutes to be deployed at higher Mach numbers and dynamic pressures. This paper demonstrates the need for expanding the parachute deployment envelope, and describes a three-phase technology development activity that has been initiated to address the need. The end result of the technology development program will be a aerodynamic decelerator system that can be deployed at Mach numbers of up to 3.1 and dynamic pressures of up to 1400 Pa. .
No associations
LandOfFree
Technology development for deployable aerodynamic decelerators at Mars does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with Technology development for deployable aerodynamic decelerators at Mars, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Technology development for deployable aerodynamic decelerators at Mars will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1086291