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Antares OA-5. Antares 230. First Antares 200 series launched on Oct 17, 2016 carrying the Enhanced Cygnus OA-5 S.S. "Alan Poindexter". 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. 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 Castor 30XL i.u.

Castor 30xl

Later missions used the Castor 30B or Castor 30XL motor. Third Stage. Future missions may The commercial igniters developed and produced will be used on GEM 63, hypersonics (CPS, MPBD), CASTOR IVB, CASTOR 30XL, and Orion motors. LCS I, LCS III, Castor 30, Castor 30XL, TO6, Castor 120, Case Builder, Testing for environmental effects on composites (hot/wet), SPAP, DTO, D5 MORA's and The CASTOR 30XL solid rocket motor measures 236 inches (6.0 m) in length and 92 inches (2.3 m) in diameter, and it weighs approximately 56,000 pounds (25,000 kg).

Antares raket – Wikipedia

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 . the NASA resupply missions, will also sup-port commercial and DOD missions.

Castor raketapp - Castor rocket stage - qaz.wiki

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. Castor 30XL.

A-ONE Antares 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. The second stage motor will burn out at approximately T+plus 6 minutes, 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. 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 … The CASTOR 30XL solid rocket motor measures 236 inches (6.0 m) in length and 92 inches (2.3 m) in diameter, and it weighs approximately 56,000 pounds (25,000 kg).
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Need to protect the Pu-238 fuel in case of an. Peacekeeper 1 Thiokol solid rocket engine. In Production. MX Stage 1. Used as first stage of Taurus launch vehicle for initial test.

Isp s.l. Thrust vac: Thrust vac: Isp vac: Burn time: Combustion: Total Imp. m: m: tons The CASTOR 30XL motor was tested at AEDC due to their unique capability of being able to simulate second stage flight conditions.
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Antares raket – Wikipedia

Images. Antares OA-5.

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Antares OA-5. Antares 230. First Antares 200 series launched on Oct 17, 2016 carrying the Enhanced Cygnus OA-5 S.S. "Alan Poindexter". A Castor 30XL could act as the third stage. This rocket would weigh 354 tonnes.

Antares raket – Wikipedia

ATK ? Castor -30XL. ATK .

Northrop Grumman named its Cygnus NG-15 spacecraft the SS Katherine Johnson in her honor. Related channels: KATHERI «Антарес» (англ. Antares) — одноразовая ракета-носитель, разработанная Orbital Sciences Corporation для запуска полезных грузов массой до 8,0 т на низкую опорную орбиту. 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).