Title:
DECELERATING DEVICE OF RE-ENTRY CAPSULE TO ATOMOSPHERE FOR SPACE PROBE
Document Type and Number:
Japanese Patent JP2833299
Kind Code:
B2
Abstract:
PURPOSE: To lessen weight and volume by lessening a mechanism for releasing a parachute.
CONSTITUTION: While a capsule 1 is formed in the center of the body 2 with an air intake port 3 extending back and forth therethrough, a rear opening of the air intake port 3 is closed with a cap 7. When the capsule 1 re-enters the atmospher, the cap 7 is released from a restricting force by air pressure coming from the air intake port 3. Further, a parachute 6 is drawn out of the capsule 1 to be opened by the cap 7 releasing energy.
More Like This:
WO/2010/139617 | LANDING SYSTEM FOR A BODY AND SPACE PROBE PROVIDED WITH SUCH A SYSTEM |
WO/2016/124591 | AEROBRAKING SATELLITE DEORBITING SYSTEM |
Inventors:
HONDA MASAHISA
Application Number:
JP29352991A
Publication Date:
December 09, 1998
Filing Date:
November 11, 1991
Export Citation:
Assignee:
NITSUSAN JIDOSHA KK
International Classes:
B64G1/62; B64D17/62; (IPC1-7): B64G1/62; B64D17/62
Other References:
【文献】米国特許3079113(US,A)
Attorney, Agent or Firm:
Fujiya Shiga (2 outside)
Previous Patent: METHOD FOR ADJUSTING SHAPE OF REFLECTING MIRROR
Next Patent: CONTROL DEVICE FOR MIXING OF HOT WATER AND WATER
Next Patent: CONTROL DEVICE FOR MIXING OF HOT WATER AND WATER