Top 10 similar words or synonyms for interstage

closest    0.986313

viewed    0.985074

cutoff    0.984581

igla    0.982101

dmitriy    0.981695

basement    0.980332

phenomenon    0.979949

labeled    0.979841

particularly    0.979777

relayed    0.978877

Top 30 analogous words or synonyms for interstage

Article Example
ဆေတန် ၅ ဒုံးပျံ For the first two unmanned launches, eight solid-fuel ullage motors ignited for four seconds to give positive acceleration to the S-II stage, followed by start of the five J-2 engines. For the first seven manned Apollo missions only four ullage motors were used on the S-II, and they were eliminated completely for the final four launches. About 30 seconds after first stage separation, the interstage ring dropped from the second stage. This was done with an inertially fixed attitude so that the interstage, only 1 meter from the outboard J-2 engines, would fall cleanly without contacting them. Shortly after interstage separation the Launch Escape System was also jettisoned. See Apollo abort modes for more information about the various abort modes that could have been used during a launch.
ဆေတန် ၅ ဒုံးပျံ Unlike the two-plane separation of the S-IC and S-II, the S-II and S-IVB stages separated with a single step. Although it was constructed as part of the third stage, the interstage remained attached to the second stage.
ဆေတန် ၅ ဒုံးပျံ A number of alternate Saturn vehicles were proposed based on the Saturn V, ranging from the Saturn INT-20 with an S-IVB stage and interstage mounted directly onto an S-IC stage, through to the Saturn V-23(L) which would not only have five F-1 engines in the first stage, but also four strap-on boosters with two F-1 engines each: giving a total of thirteen F-1 engines firing at launch.
ဆေတန် ၅ ဒုံးပျံ Five level sensors in the bottom of each S-II propellant tank were armed during S-II flight, allowing any two to trigger S-II cutoff and staging when they were uncovered. One second after the second stage cut off it separated and several seconds later the third stage ignited. Solid fuel retro-rockets mounted on the interstage at the top of the S-II fired to back it away from the S-IVB. The S-II impacted about from the launch site
ဆေတန် ၅ ဒုံးပျံ Acceleration increased during S-IC flight for two reasons: decreasing propellant mass, and increasing thrust as F-1 engine efficiency improved in the thinner air at altitude. At 135 seconds, the inboard (center) engine shut down to limit acceleration to 4 "g" (39.2 m/s). The other engines continued to burn until either oxidizer or fuel depletion is detected by sensors in the suction assemblies. First stage separation was a little less than one second after cutoff to allow for F-1 thrust tail-off. Eight small solid fuel separation motors backed the S-IC from the interstage at an altitude of about . The first stage continued ballistically to an altitude of about and then fell in the Atlantic Ocean about downrange.