| 词条 | 1.5KS35000 |
| 释义 |
|image= |image_size= |caption= |name=1.5KS35000 |country_of_origin=United States |designer=Thiokol |manufacturer= |date= |purpose= |predecessor= |status=Retired |cycle= |type=solid |fuel= |oxidiser= |capacity= |combustion_chamber= |nozzle_ratio= |thrust(SL)= |thrust(Vac)=156 kN |specific_impulse_vacuum= |specific_impulse_sea_level= |chamber_pressure= |thrust_to_weight= |diameter=0.23 m |length=2.60 m |dry_weight= }}1.5KS35000 is a solid propellant rocket engine designed by Thiokol and used in the experimental Recruit rocket. It was used in at least 23 launches.[1][2] References1. ^{{Cite web | last = McDowell| first = Jonathan | title = Stages| work = | publisher = | date = February 2007| url = http://www.planet4589.org/space/lvdb/sdb/Stages| format = | doi = | accessdate = 2010-03-02}} {{Suborbital rocket engines}}{{rocket-stub}}2. ^1.5KS35000 1 : Rocket engines |
| 随便看 |
|
开放百科全书收录14589846条英语、德语、日语等多语种百科知识，基本涵盖了大多数领域的百科知识，是一部内容自由、开放的电子版国际百科全书。