Computer Science – Sound
Scientific paper
Jun 1980
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980esasp.152..189h&link_type=abstract
In ESA European Rocket and Balloon Programs and Related Res. p 189-197 (SEE N81-10914 01-99)
Computer Science
Sound
Failure Analysis, Heat Sinks, Rocket Vehicles, Sounding Rockets, Aluminum, Heat Transfer, High Gravity Environments, Minuteman Icbm, Performance Tests, Solid Propellant Rocket Engines, Temperature Effects, Thermal Insulation, Titanium
Scientific paper
The failure analysis performed for ARIES sounding rocket motor failures, and the remedy developed for motor overheating are described. The principal failure hypothesis was that the motor-dome insulator fails under high gravity boost and the subsequent radiant heating of the titanium motor dome weakens the pressure vessel. The supporting heat transfer and ablation analyses are summarized. These detailed analyses and digital simulations quantitatively correlated the precise time-of-failure with known ablation and heat transfer rates and established firm design criteria for the aluminum heat sink. Analysis of the international magnetospheric study test rocket temperature data is described. This analysis confirmed the validity of the design and the effectiveness of the heat sink.
Haerendel Gerhard
Jerger J. H.
Jerger J. J.
No associations
LandOfFree
The Aries heat sink 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 The Aries heat sink, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and The Aries heat sink will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1216510