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Class Information
Number: 244/159.1
Name: Aeronautics > Spacecraft > Reusable or returnable > With reentry shield
Description: Subject matter in which the means to ensure includes specific means for protection of the spacecraft due to motion through the atmosphere of the celestial body.
Sub-classes under this class:
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7546982 |
Shuttle thermal integrity detection system |
Jun. 16, 2009 |
| 7407131 |
Method for creating an aeronautic sound shield having gas distributors arranged on the engines, wings, and nose of an aircraft |
Aug. 5, 2008 |
| 7392964 |
Method and apparatus for utilizing a lifeboat for a space station in earth orbit to serve as a lunar spacecraft |
Jul. 1, 2008 |
| 7381459 |
Toughened uni-piece, fibrous, reinforced, oxidization-resistant composite |
Jun. 3, 2008 |
| 7377469 |
Heat shield |
May. 27, 2008 |
| 7281688 |
Materials for self-transpiring hot skins for hypersonic vehicles or reusable space vehicles |
Oct. 16, 2007 |
| 7267303 |
Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy |
Sep. 11, 2007 |
| 7237752 |
System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping |
Jul. 3, 2007 |
| 7229048 |
Aerodynamic control of a hypersonic entry vehicle |
Jun. 12, 2007 |
| 7219859 |
Multipurpose modular spacecraft |
May. 22, 2007 |
| 7198231 |
Method of applying ablative insulation coatings and articles obtained therefrom |
Apr. 3, 2007 |
| 7195207 |
Winged spacecraft |
Mar. 27, 2007 |
| 6886790 |
Stand-off for fixing thermal protection panels |
May. 3, 2005 |
| 6844057 |
Method for secondarily bonding a ceramic matrix composite layer to a flexible insulation blanket and an insulation blanket produced thereby |
Jan. 18, 2005 |
| 6827312 |
Method and system of thermal protection |
Dec. 7, 2004 |
| 6607851 |
Multi-layer ceramic fiber insulation tile |
Aug. 19, 2003 |
| 6592981 |
Oxidation resistant insulating sandwich tiles |
Jul. 15, 2003 |
| 6530543 |
Hypersonic and orbital vehicles system |
Mar. 11, 2003 |
| 6505794 |
Large thermal protection system panel |
Jan. 14, 2003 |
| 6467731 |
Integrated sample return capsule |
Oct. 22, 2002 |
| 6257527 |
Hypersonic and orbital vehicles system |
Jul. 10, 2001 |
| 6241184 |
Vehicle having a ceramic radome joined thereto by an actively brazed compliant metallic transition element |
Jun. 5, 2001 |
| 6136418 |
Rapidly removable thermal protection system for reusable launch vehicle |
Oct. 24, 2000 |
| 6013361 |
High performance structural laminate composite material for use to 1000.degree. F and above, apparatus for and method of manufacturing same, and articles made with same |
Jan. 11, 2000 |
| 5882765 |
Element made of a reinforced low density heat protective material and method to obtain said element |
Mar. 16, 1999 |
| 5772154 |
Leading edge heat shield for wings of spacecraft |
Jun. 30, 1998 |
| 5649488 |
Non-explosive target directed reentry projectile |
Jul. 22, 1997 |
| 5560569 |
Aircraft thermal protection system |
Oct. 1, 1996 |
| 5511747 |
Arrangement for thermal protection of an object, such as a thermal shield |
Apr. 30, 1996 |
| 5489074 |
Thermal protection device, in particular for an aerospace vehicle |
Feb. 6, 1996 |
| 5457471 |
Adaptively ablatable radome |
Oct. 10, 1995 |
| 5452866 |
Transpiration cooling for a vehicle with low radius leading edge |
Sep. 26, 1995 |
| 5413859 |
Sublimitable carbon-carbon structure for nose tip for re-entry space vehicle |
May. 9, 1995 |
| 5351917 |
Transpiration cooling for a vehicle with low radius leading edges |
Oct. 4, 1994 |
| 5340058 |
Projectile with cooled nose cone |
Aug. 23, 1994 |
| 5330124 |
Thermal protection device using the vaporization and superheating of a rechargeable liquid |
Jul. 19, 1994 |
| 5312685 |
Atomic oxygen protective coating with resistance to undercutting at defect sites |
May. 17, 1994 |
| 5310592 |
Fibrous ceramic aerobrake |
May. 10, 1994 |
| 5291830 |
Dual-mode semi-passive nosetip for a hypersonic weapon |
Mar. 8, 1994 |
| 5265829 |
Tetrahedral lander |
Nov. 30, 1993 |
| 5257757 |
Advanced hypersonic nosecap |
Nov. 2, 1993 |
| 5254837 |
Thermally activated retainer means utilizing shape memory alloy |
Oct. 19, 1993 |
| 5236151 |
Thermal barrier structure |
Aug. 17, 1993 |
| 5217185 |
Ablative shielding for hypervelocity projectiles |
Jun. 8, 1993 |
| 5209896 |
Heat shield |
May. 11, 1993 |
| 5178922 |
Fringed thermal protection device |
Jan. 12, 1993 |
| 5117606 |
Structural member |
Jun. 2, 1992 |
| 5108830 |
Shape-stable reentry body nose tip |
Apr. 28, 1992 |
| 4966229 |
Leading edge heat pipe arrangement |
Oct. 30, 1990 |
| 4961384 |
Hypervelocity penetrator for an electromagnetic accelerator |
Oct. 9, 1990 |
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