Top 10 similar words or synonyms for parking

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veteran    0.978451

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Top 30 analogous words or synonyms for parking

Article Example
ဆလီနီအာကာသယာဉ် ဆလီနီအာကာသယာဉ်ကို ၂၀၀၇ခုနှစ်၊ စက်တင်လာလ ၁၄ရက်နေ့တွင် 01:31:01 UTC တွင် H-IIA (Model H2A2022) သယ်ယူပို့ဆောင်ရေးဒုံးပျံဖြင့် Tanegashima Space Center မှ---into a (perigee) / (apogee) geocentric parking orbit. The total launch mass was .
ဆေတန် ၅ ဒုံးပျံ This parking orbit was quite low by Earth orbit standards, and it would have been short-lived due to aerodynamic drag. This was not a problem on a lunar mission because of the short stay in the parking orbit. The S-IVB also continued to thrust at a low level by venting gaseous hydrogen, to keep propellants settled in their tanks and prevent gaseous cavities from forming in propellant feed lines. This venting also maintained safe pressures as liquid hydrogen boiled off in the fuel tank. This venting thrust easily exceeded aerodynamic drag.
ဆေတန် ၅ ဒုံးပျံ During Apollo 11, a typical lunar mission, the third stage burned for about 2.5 minutes until first cutoff at 11 minutes 40 seconds. At this point it was   downrange and in a parking orbit at an altitude of   and velocity of 17,432 mph. The third stage remained attached to the spacecraft while it orbited the Earth two and a half times while astronauts and mission controllers prepared for translunar injection (TLI).
ဆေတန် ၅ ဒုံးပျံ For the final three Apollo flights, the temporary parking orbit was even lower (approximately ), to increase payload for these missions. The Apollo 9 Earth orbit mission was launched into the nominal orbit consistent with Apollo 11, but the spacecraft were able to use their own engines to raise the perigee high enough to sustain the 10-day mission. The Skylab was launched into a quite different orbit, with a perigee which sustained it for six years, and also a higher inclination to the equator (50 degrees versus 32.5 degrees for Apollo).
ဆေတန် ၅ ဒုံးပျံ The S-IVB-500 model used on the Saturn V differed from the S-IVB-200 used as the second stage of the Saturn IB, in that the engine was restartable once per mission. This was necessary as the stage would be used twice during a lunar mission: first in a 2.5 min burn for the orbit insertion after second stage cutoff, and later for the trans-lunar injection (TLI) burn, lasting about 6 min. Two liquid-fueled Auxiliary Propulsion System (APS) units mounted at the aft end of the stage were used for attitude control during the parking orbit and the trans-lunar phases of the mission. The two APSs were also used as ullage engines to settle the propellants in the aft tank engine feed lines prior to the trans-lunar injection burn.