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Antares raket – Wikipedia

The third digit denotes the type of third stage used. 0 indicates that no third stage is present, 1 indicates a Bi-Propellant Third Stage (BTS) powered by nitrogen tetroxide and hydrazine, and 2 indicates a solid-fueled Star-48 -based third stage. 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.

ARNOLD AIR FORCE BASE, Tenn. -- Testing is complete on an Alliant Techsystems, Inc.'s (ATK) CASTOR® 30XL developmental rocket motor in AEDC's J-6 Large Rocket Motor Testing Facility. "AEDC is the only place to test this motor, due to their unique capability of being able to simulate upper atmospheric conditions," said Jeff Winter, ATK program manager for CASTOR® 30XL. 2013-03-05 Castor 30 – Photo: Orbital ATK. The Castor 30XL Upper Stage of the inaugural mission of the Antares 230 launch vehicle re-entered the atmosphere on November 6, 2016 after only three weeks in orbit following the successful launch of the Cygnus OA-5 cargo … The solid propellant Castor 30XL upper stage of Antares, seen here in processing for the NG-12 mission later in 2019. (Credit: Brady Kenniston) “So the way PEG works is it keeps monitoring that 2018-11-17 2014-10-27 2021-02-20 The CASTOR 30XL is a high-performing upper stage motor in ATK's commercial product line of solid rocket motors. The company's flight-proven rocket motors are utilized for military and commercial Castor 30XL was successfully test fired for the first time on March 28, 2013 at the U.S. Air Force's Arnold Engineering Development Complex (AEDC) in Tennessee. Orbital planned to establish a new Taurus II west coast launch site that would be ready in 2014.

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scheduled to fly on the fifth flight of Antares (ORB-3). Quinn said the new motor being tested at AEDC, besides its application to help with .

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Richard Kirkpatrick, AEDC’s project . manager for the test, and Quinn emphasized The second stage on the other hand is a Castor-30XL solid rocket motor. Fueled by hydroxyl-terminated polybutadiene (HTPB) and aluminum, it produces 474 kN (~107,000 lbf) of thrust. An Antares 230+ rocket prior to liftoff of the CRS-2 NG-13 mission.

Diameter: 2.36 m. Engine: Castor 30XL Fuel: TP-H8299/aluminium. Thrust: 474 kN (107,000 lbf) Burn Time: 156 seconds 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 Peacekeeper 1 Thiokol solid rocket engine. In Production. MX Stage 1.
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These motors could be the same 3.71 meter diameter as the SLS and Stratolaunch solid rocket motors. 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.

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The company's flight-proven rocket motors are utilized for military and commercial customer missions. A basic version of the CASTOR 30 motor was tested at AEDC in December 2009 and will fly the initial Antares missions. The Castor 30XL second stage SRM produces 293.4 kN of thrust and burns for 156 seconds. Vehicle Status Orbital ATK is currently launching Cygnus cargo vehicles to the ISS aboard United Launch CASTOR Motors.