| 词条 | 1.8KS7800 |
| 释义 |
|image= |image_size= |caption= |name=1.8KS7800 |country_of_origin=United States |designer=Aerojet |manufacturer= |date=1957 |purpose= |predecessor= |status=Retired |cycle= |type=solid |fuel= |oxidiser= |capacity= |combustion_chamber= |nozzle_ratio= |thrust(SL)= |thrust(Vac)=35 kN |specific_impulse_vacuum= |specific_impulse_sea_level= |chamber_pressure= |thrust_to_weight= |diameter=0.2 m |length=1.3 m |dry_weight= }}1.8KS7800 is a solid propellant rocket engine designed by Aerojet and used in the AIM-7A, AIM7B and AIM7C Sparrow missiles.[1] The designation 1.8KS7800 means that the engine burns during 1.8 seconds and generates 7,800 pounds of thrust.[2][3][4] References1. ^{{Cite web | last = Parsch| first = Andreas| title = Raytheon AAM-N-2,3,6/AIM-101/AIM-7/RIM-7 Sparrow| date = April 7, 2007| url = http://www.designation-systems.net/dusrm/m-7.html| accessdate = March 2, 2010}} {{rocket-stub}}2. ^{{Cite web | title = Rocket Motor, Solid Fuel, 1.KS 7800, Sparrow II Missile| publisher = Smithsonian National Air and Space Museum| url = http://www.nasm.si.edu/collections/artifact.cfm?id=A19590099003| accessdate = March 2, 2010}} 3. ^{{Cite web | last = Wade| first = Mark| title = 1.8KS7800| date = 2008| url = http://www.astronautix.com/engines/18ks7800.htm| accessdate = March 2, 2010}} 4. ^{{Cite web | last = McDowell| first = Jonathan| title = Stages| date = February 2007| url = http://www.planet4589.org/space/lvdb/sdb/Stages| accessdate = 2010-03-02}} 1 : Rocket engines |
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