Top 10 similar words or synonyms for accelerated

profiler    0.957090

autocomplete    0.956817

buzz    0.955563

refactoring    0.955424

sistema    0.954294

shutdown    0.954061

activestate    0.952273

toolkit    0.952008

toolchain    0.951095

messaging    0.950274

Top 30 analogous words or synonyms for accelerated

Article Example
ပလေးစတေရှင် ၄ ပလေးစတေရှင် ၄ ဂိမ်းစက်သည် AMD x86-64 Accelerated Processing Unit ကိုအသုံးပြုထားကာ ဂိမ်းရေးဆွဲဖန်တီးသူများအား ဆွဲဆောင်ထားသည်။ ဆိုနီမှ ပလေးစတေရှင် ၄ ဂိမ်းစက်အား "ကမ္ဘာ့စွမ်းအားအမြင့်ဆုံးဂိမ်းစက်" အဖြစ် တင်စားခေါ်ဝေါ်ခဲ့သည်။ များစွာသော ဂိမ်းဖန်တီးသူတို့က အိပ်စ်ဘောက်စ်ဝမ်းနှင့် ပီအက်စ်ဖိုး တို့၏စွမ်းဆောင်မှုသည် သိသိသာသာကွာခြားသည်ဟု ဆိုကြောင်း ဆိုနီမှ မဂ္ဂဇင်းသို့ ပြောကြားခဲ့သည်။
ဟော်တင်ဟို ၂၂၉ လေယာဉ် Despite this setback, the project continued with sustained energy. On 12 March 1945, the Ho 229 was included in the "Jäger-Notprogramm" (Emergency Fighter Program) for accelerated production of inexpensive "wonder weapons". The prototype workshop was moved to the Gothaer Waggonfabrik (Gotha) in Friedrichroda. In the same month, work commenced on the third prototype, the Ho 229 V3.
ပိုင်အိုနီးယား-၁၀ အာကာသယာဉ် The "Pioneer 10" probe was launched on March 3, 1972 at 01:49:00 UTC (March 2 local time) by the [[National Aeronautics and Space Administration]] from [[Cape Canaveral Air Force Station Space Launch Complex 36|Space Launch Complex 36A]] at [[Cape Canaveral Air Force Station|Cape Canaveral]], Florida aboard an [[Atlas-Centaur|Atlas/Centaur]] launch vehicle. The third stage consisted of a solid fuel [[TE364-4]] developed specifically for the Pioneer missions. This stage provided about 15,000 pounds of thrust and spun up the spacecraft. The spacecraft had an initial spin rate of 30 revolutions per minute. Twenty minutes following the launch, the vehicle's three booms were extended, which slowed the rotation rate to 4.8 per minute. This rate was maintained throughout the voyage. The launch vehicle accelerated the probe for net interval of 17 minutes, reaching a velocity of 51,682 kilometers/hour (32,114 miles/hour).
ဆေတန် ၅ ဒုံးပျံ The S-II was built by North American Aviation at Seal Beach, California. Using liquid hydrogen and liquid oxygen, it had five J-2 engines in a similar arrangement to the S-IC, also using the outer engines for control. The S-II was tall with a diameter of , identical to the S-IC, and thus was the largest cryogenic stage until the launch of the STS. The S-II had a dry weight of about and fully fueled, weighed . The second stage accelerated the Saturn V through the upper atmosphere with of thrust (in vacuum). When loaded, significantly more than 90 percent of the mass of the stage was propellant; however, the ultra-lightweight design had led to two failures in structural testing. Instead of having an intertank structure to separate the two fuel tanks as was done in the S-IC, the S-II used a common bulkhead that was constructed from both the top of the LOX tank and bottom of the LH2 tank. It consisted of two aluminum sheets separated by a honeycomb structure made of phenolic resin. This bulkhead had to insulate against the temperature difference between the two tanks. The use of a common bulkhead saved . Like the S-IC, the S-II was transported by sea.