Antares raket - qaz.wiki

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Another Double Header Attempt First attempt: A Northrop Grumman Antares rocket will launch the 15th Cygnus cargo freighter on the 14th operational cargo delivery flight to the International Space 11 Apr 2013 Testing is complete on an Alliant Techsystems, Inc.'s (ATK) CASTOR® 30XL developmental rocket motor in AEDC's J-6 Large Rocket Motor On April 25, 2011, Orbital announced that it had directed ATK to develop a more powerful upper stage named "Castor 30XL". The $57 million effort would of Antares is liquid-propellant, burning RP-1 kerosene (fuel) and liquid oxygen (oxidizer). The second stage uses a Castor-30XL solid-propellant rocket motor. 28 Mar 2013 ATK successfully ground tested its new CASTOR 30XL upper stage solid rocket motor March 27, 2013, at the U.S. Air Force's Arnold The rocket flies in the Antares 230 configuration, with two RD-181 first stage engines and a Castor 30XL second stage. Launch site: MARS (Mid-Atlantic 20 Feb 2021 Cygnus spacecraft separated to reveal the spacecraft and the interstage, which surrounded the Castor 30XL, fell away before the solid motor 26 Nov 2017 Castor 30 – Photo: Orbital ATK. The Castor 30XL Upper Stage of the second mission of the Antares 230 launch vehicle re-entered the These show powered Jupiter flyby results for CASTOR 30B and CASTOR 30XL kick stage configurations, respectively, with the similar payload mass variations. On to the Castor 30XL.pic.twitter.com/eXARDRrRVx. 1:49 AM - 21 May 2018.

Den ursprungliga designen av Castor 30XL byggdes konservativt och efter att ha fått CASTOR motor variations support Northrop Grumman Minotaur-C vehicles, and the latest generation CASTOR 30XL motor propels the upper stage of Antares for cargo resupply missions to the International Space Station. The CASTOR 30XL is a low-cost, robust, state-of-the-art upper stage motor. CASTOR 30XL is more than a stretched version of the CASTOR 30. The motor also capitalizes on existing common designs and materials, plus lessons learned while developing the Large Class Stage I and III. Castor 30XL Photos: Antares blasts off from Virginia October 8, 2020 A Northrop Grumman Antares launched from Virginia’s Eastern Shore with a commercial Cygnus supply ship Oct. 2 on a Richard Kirkpatrick, AEDC's project manager for the test, and Quinn emphasized that the CASTOR 30XL motor is designed to provide greater payload for cargo resupply missions to the International Space Station. The test measured thrust, pressure and burn rate, all of which depended on the internal pattern of the propellant during the firing in J-6. Category: Castor 30XL. October 8, 2020 Photos: Antares blasts off from Virginia.

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The launcher’s Castor 30XL solid-fueled upper stage will ignite at T+plus 4 minutes, 7 seconds, and generate up to 104,300 pounds of thrust during a burn lasting approximately 2 minutes, 45 seconds. Castor 30XL –Star 48BV •EUS to Castor 30XL •3470 lb + 625 lb (MGA) = 4095 lb adapter predicted mass •Dimensions: 154.0 in tall, 331.0 in base, 95.0 in top •Supporting 85,384 lbs including Castor 30XL, Star 48BV, and 10 mt payload •154.0 in to clear EUS fwd dome, vent valve, and nozzle •Castor 30XL to Star 48BV The CASTOR 30XL solid rocket motor is 92 inches in diameter, 236 inches in length and weighs approximately 58,000 lbs. The nozzle is eight feet long with a submerged design with a high Castor 30XL i.u.

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Castor 30XL Test Firing – Photo: Orbital ATK. The second stage, an Orbital ATK Castor 30XL solid rocket motor, is a larger version of the Castor 30 used on the first three missions of the Antares rocket and was planned to be first used on the Cygnus Orb-3 mission. The CASTOR 30XL solid rocket motor is 92 inches in diameter, 236 inches in length and weighs approximately 58,000 pounds. The nozzle is eight feet long with a submerged design with a high A Castor-30A second stage helps propel the first two Antares-110 rockets into orbit, then a higher-performing Castor-30B motor was used with the Antares-120 on the third and fourth flights in 2013. On the fifth flight, the stretched Castor-30XL upper stage was introduced on the Antares-130.

This rocket would weigh about 355 tonnes at liftoff, but could be slightly shorter then the existing Antares. V prvních dvou letech Antaru bude použita verze Castor 30A, další dvě rakety Antares použijí vylepšenou verzi Castor 30B. V následujících letech bude používán větší Castor 30XL. Průměr hlavy rakety s nákladem je také 3,9 m, výška 9,9 m. The Castor 30XL was on the previous Antares launch but didn't get a chance to fire because of the first stage failure, so this was its first real test. In the event the rocket performed above specification and the mission reached a higher-than-planned 209 x 351 km orbit.
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Related channels: KATHERI 2011-04-25 · ATK announced Monday that the company was awarded a $57 million contract to provide the CASTOR 30XL — an upgraded second stage motor for Orbital Science Corporation's Taurus II commercial launch vehicle — which will supply cargo for NASA to the International Space Station.

Third stage Första steget bestod av två stycken AJ26-62, andra steget av en Castor 30B och inget tredje steg. Den flög första gången den 9 januari 2014.
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Castor 30XL –Star 48BV •EUS to Castor 30XL •3470 lb + 625 lb (MGA) = 4095 lb adapter predicted mass •Dimensions: 154.0 in tall, 331.0 in base, 95.0 in top •Supporting 85,384 lbs including Castor 30XL, Star 48BV, and 10 mt payload •154.0 in to clear EUS fwd dome, vent valve, and nozzle •Castor 30XL to Star 48BV The Castor 30XL was on the previous Antares launch but didn't get a chance to fire because of the first stage failure, so this was its first real test. In the event the rocket performed above specification and the mission reached a higher-than-planned 209 x 351 km orbit. The launcher’s Castor 30XL solid-fueled upper stage will ignite at T+plus 4 minutes, 7 seconds, and generate up to 104,300 pounds of thrust during a burn lasting approximately 2 minutes, 45 seconds. Castor 30XL i.u.

Oct 18, 2016 Stage II thrust (Castor-30XL). 464 kilonewtons (average) 533 kilonewtons ( maximum). Stage II burn time (Castor-30XL). ~163 seconds The Castor 30XL solid-fuel rocket engine powers the second stage of the Antares launch vehicle.