Self-propelled rocket and collapsible rocket launch stand...

F - Mech Eng,Light,Heat,Weapons – 42 – B

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

F42B 15/00 (2006.01) F41F 3/045 (2006.01) F42D 3/00 (2006.01)

Patent

CA 2408821

A self-propelled and constant-acceleration rocket (10) for use in triggering an avalanche includes a hollow cylindrical body member having an interior volume, an open top end, and an open bottom end whose exterior surface includes a plurality of flight guidance fins (15). A partition wall (30) divides the interior volume into an upper volume and a lower volume. An explosive payload (13) is mounted within the upper volume, and a nose cone (11) having a circular and planar tip closes the open top end of the body member. A rocket motor is mounted within the lower volume. The rocket has a center of gravity (6) and a center of pressure (cp) that are both located on the rocket's central axis and within the lower volume. The center of gravity is located closer to the open top end than is the center of pressure. A collapsible launch stand holds the rocket in a launch tube for launching of the rocket. Adjustment of a pair of launch tube support members provides for adjustment of the rocket's launch angle.

Cette invention a trait à une fusée autopropulsée à accélération constante utilisable pour déclencher une avalanche. Cette fusée est constituée d'un corps creux cylindrique, comportant un volume intérieur, une extrémité avant ouverte ainsi qu'une extrémité arrière ouverte dont la surface extérieure est pourvue d'ailerons de guidage du vol. Un cloison subdivise le volume intérieur en deux volumes, supérieur et inférieur. Une coiffe ayant une tête circulaire et plate obture l'extrémité avant ouverte du corps de la fusée. Un moteur est placé dans le volume inférieur de la fusée. Le centre de gravité et le centre de pression se trouvent tous deux sur l'axe central de la fusée et à l'intérieur du volume inférieur. Le centre de gravité est plus proche de l'extrémité avant ouverte que ne l'est le centre de pression. Un poste de tir repliable maintient la fusée dans un tube de tir destiné au lancement de celle-ci. Le réglage de deux éléments de support du tube de tir permet d'obtenir l'angle de tir de la fusée.

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

Self-propelled rocket and collapsible rocket launch stand... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Self-propelled rocket and collapsible rocket launch stand..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Self-propelled rocket and collapsible rocket launch stand... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1474711

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.