Engine: Castor 30XL Fuel: TP-H8299/aluminium Thrust: 474 kN (107,000 lbf) Burn Time: 156 seconds. Stage 3 – Star-48BV (Optional) Length: 1.24 m Diameter: 2.08 m

Designation. Motor: Length: Diam. Mass: Propellant: Thrust s.l. Thrust s.l. Isp s.l. Thrust vac: Thrust vac: Isp vac: Burn time: Combustion: Total Imp. m: m: tons

2013-03-29 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. First Antares launch using Castor 30XL. Cygnus "Deke Slayton". Launched on Oct 28, 2014 but rocket encountered anomaly and exploded.

Första steget bestod av två stycken AJ26-62, andra steget av en Castor 30XL och inget tredje steg. 3, 2 × RD-181, Castor 30XL, i.u. Första steget bestod av två stycken AJ26-62, andra steget av en Castor 30XL och inget tredje steg. Den flög PP 30 XL 037 FM / FF 2 48.51 48.00 40 51.0 11 2.5 13.5 25.0 25 11.5. PP 32 XL R.P.M.

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.

Stage 3 – Star-48BV (Optional) Length: 1.24 m Diameter: 2.08 m 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. Over the next minute, the payload fairing encapsulating the Cygnus spacecraft separated to reveal the spacecraft and the interstage, which surrounded the Castor 30XL, fell away before the solid 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.

Den femte flygningen var av konfigurationen Antares 130. Första steget bestod av två stycken AJ26-62, andra steget av en Castor 30XL och inget tredje steg.

The Antares 230 rocket for this mission is a two-stage launch Castor -120. ATK. 7.67, 2.36, 53.078, 49.006, 1,694.0, 1,528.9, 2481, 1,868.0, 1,685.9, 2736, 79.5, 0.6162, 134.071. Castor -120XL. ATK ? Castor -30XL.

Isp s.l. Thrust vac: Thrust vac: Isp vac: Burn time: Combustion: Total Imp. m: m: tons Thiokol previously supplied solid motors for OSC's previous launchers such as the air-launched Pegasus and the ground-based Minotaur and Taurus-1. Eventually, the 30B and 30XL variants of the Castor motor were developed. Theoretically, the Taurus-2 could be equipped with a third stage, which could use storable liquid propellant. Launch pad Castor 30XL would serve as the third stage. 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.
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The CASTOR 30XL is based on the CASTOR 120, used in more than a dozen missions.

Den flög första gången den 9 januari 2014. 130.
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Castor 30XL would serve as the third stage. 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.

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.

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CASTOR 30XL VECTORABLE NOZZLE IN-LINE UPPER STAGE BOOSTER 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.

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 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. 1 indicates a Castor-30A, 2 a Castor-30B, and 3 a Castor-30XL. 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.