Ракетный блок. Castor 30B. [Редактировать]

Технические характеристики

#ХарактеристикаЗначение
1Длина, метра4.17
2Стартовая масса, кг13970
3ТопливоHTPB H8299
4Тяга (средняя), кНьютон293.4
5Тяга (максимальная), кНьютон396.3
6Удельный импульс, секунд76
7Время работы, секунд127
8Масса (топлива), кг12887
9Диаметр, метра2.34
10Давление (в камере сгорания), бар53

Найдено 40 документов по запросу «Castor 30B». [Перейти к поиску]


Дата загрузки: 2017-02-22
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0.04/5
... in the STAR™, Orion, and CASTOR® series, for instance). Orbital ATK... CASTOR MOTOR SERIES ............................................................................................. 23 CASTOR IVA ....................................................................................................... 24 CASTOR IVA-XL .................................................................................................. 25 CASTOR IVB ....................................................................................................... 26 CASTOR 30 ......................................................................................................... 27 CASTOR 30B ....................................................................................................... 28 CASTOR... Space Propulsion Product portfolio: Orion, ® ® CASTOR , CASTOR 120 , LCS (large class stage... trademarks of Orbital ATK. CASTOR and CASTOR 120 are registered trademarks of... Contact No. STAR, ASAS, and CASTOR I and II Motors; STAR™ Stages... LARGE MOTOR SUMMARY INFORMATION ORION, CASTOR, LCS, GEM, AND RSRM MOTOR... ATK’s large motor series (Orion, CASTOR, LCS, GEM, and RSRM families... 32 ORION 50XL CASTOR 120 ORION 50 CASTOR 30 ORION 38 1900... XLT Orion 50S XLG CASTOR Motor Family CASTOR IVA Vectorable Fixed Vectorable... Flight-proven Flight-proven CASTOR IVA-XL CASTOR IVB Fixed 40.1 363....0 63.6 Flight-proven Flight-proven CASTOR 30 Vectorable 92 138 28...,565 0.92 8,236,000 153.4 CASTOR 30B Vectorable 92 164 28,412....7 Qualified at simulated altitude Qualified CASTOR 120 *Large Class Stage (LCS... XLG Orion 50S XLT CASTOR IVA CASTOR IVB CASTOR IVA-XL Applications/Uses... Space Propulsion Products Catalog Motor CASTOR 30 CASTOR 30B CASTOR 120 LCS I LCS III... Catalog  CASTOR MOTOR SERIES LOW-COST, HIGH-RELIABILITY BOOSTERS The CASTOR motor... booster for Delta II. The CASTOR I-IV family has a combined total... CASTOR IVA, IVA-XL, and IVB have replaced the CASTOR IV motor.    CASTOR IVA, high-performance strap-on propulsion launch vehicles CASTOR... with 30% greater launch capability CASTOR IVB, TVC version with first... launches carry commercial satellites and CASTOR motors are designed to provide... CASTOR series. Development of the CASTOR 120 motor began in 1989. The CASTOR... rating and a 50% cost reduction. CASTOR 120 motors have served as... upper stage CASTOR 30/30B has been added to the series. CASTOR 30...-S-1902; Dated 07 August 2012 CASTOR IVA MOTOR DIMENSIONS Motor diameter... FIXED NOZZLE PROPELLANT DESIGNATION The CASTOR IVA motor was developed in... HTPB propellant (from the earlier CASTOR IV), NASA was able to.... Each Delta vehicle carried nine CASTOR IVA strap-on motors until... the Conestoga in October 1995. CASTOR IVA motors have also flown... STATUS .....Flight proven, inactive production CASTOR® IVA Vaccum Thrust vs. Time... The CASTOR IVA-XL motor, an 8-foot extension of the CASTOR IVA... H-IIA launch vehicle uses modified CASTOR IVA-XL motors with 6-degree... and vehicle configuration. The first CASTOR IVA-XL SSB motors flew... STATUS .....Flight proven, inactive production CASTOR® IVA-XL Vaccum Thrust vs...; Dated 07 August 2012 25 CASTOR IVB MOTOR DIMENSIONS Motor diameter... CASTOR IVB motor was the first in the series of CASTOR IVA... boost on all MAXUS flights. CASTOR IVB motors have also served...°-100°F PRODUCTION STATUS ................... Flight proven CASTOR® IVB Vaccum Thrust vs. Time...; Dated 07 August 2012 26 CASTOR 30 MOTOR DIMENSIONS Motor diameter... STAGE BOOSTER HAZARDS CLASSIFICATION… ...................1.3 The CASTOR 30 is a low cost, robust... configuration. The design of the CASTOR 30 uses all flight-proven...…. ................................................+30°-105°F PRODUCTION STATUS ...................... Production CASTOR® 30 Vaccum Thrust vs. Time...; Dated 07 August 2012 27 CASTOR 30B MOTOR DIMENSIONS Motor diameter, in... STAGE BOOSTER HAZARDS CLASSIFICATION…. ..................1.3 The CASTOR 30B is a low cost, robust, state... incorporates a few modifications from the CASTOR 30, primarily a change in propellant...°-105°F PRODUCTION STATUS ............... In production CASTOR® 30B Vaccum Thrust vs. Time 100000...; Dated 07 August 2012 28 CASTOR 120 MOTOR DIMENSIONS Motor diameter... VECTORABLE NOZZLE HAZARDS CLASSIFICATION….. .................1.3 The CASTOR 120 was designed, using proven... component development and qualification supporting CASTOR 30 motors. Burn time, sec... component development and qualification supporting CASTOR 30 motors. Motor diameter, in... Orbital ATK’s STAR, ASAS, Orion, CASTOR, GEM, and RSRM motors span... of our successful STAR and CASTOR series of motors. It incorporates... booster destruct applications on STAR, CASTOR, Titan, Atlas, and Delta Semiconductor...



Дата загрузки: 2016-10-31
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0.56/5
... stage relies on proven ATK CASTOR solid rocket motors and Orbital... 2.2.1-1. Antares Main Engine System .............................................................................................. 4 Figure 2.2.2-1. CASTOR 30B Motor ............................................................................................................ 5 Figure 2.2.3.1-1. Antares 3.9 m Fairing Assembly... configurations (Figure 2.2-2) utilize the CASTOR 30B and CASTOR 30XL SRM second stage, respectively... (CASTOR) Both the CASTOR 30B and CASTOR 30XL second 120 (Baseline) LOX/RP, AJ26 30B.../RP, AJ26 30B BTS (ATK), are based on the CASTOR 30 SRM. The 122 (Enhanced) LOX/RP, AJ26 30B STAR... BTS al length of the CASTOR 30XL SRM. This adapter 132... 2.2.2. Stage 2 Assembly Orbital uses the CASTOR 30 family of SRMs as...). The CASTOR 30 product line is derived from the heritage CASTOR 120 motor used on the Taurus launch vehicle. The CASTOR... CASTOR motor aft skirt. Figure 2.2.2-1. CASTOR 30B Motor Antares utilizes variants of the CASTOR... the CASTOR 30B motor (Antares 120). An enhancement offered includes the CASTOR 30XL motor (Antares 130). Both the CASTOR 30B and CASTOR 30XL motors are derived from the CASTOR 30 but... by the combination of the CASTOR 30 TVC and the onboard... Antares 120 vehicle with the CASTOR 30B second stage from WFF to... total impulse errors from the CASTOR 30B and 30XL motors, respectively. The... performance of the Antares vehicle: a CASTOR 30XL SRM second stage and... SRM third stage. 8.13.1. Antares CASTOR 30XL Second Stage For enhanced... LOX/RP-1 first stage and a CASTOR 30XL SRM second stage. As... 120 using the higher impulse CASTOR 30XL. The Antares 130 utilizes... the additional length of the CASTOR 30XL SRM. This adapter allows... for the Antares 120. The CASTOR 30XL SRM is loaded with... CASTOR 30XL SRM utilizes heritage components and designs common to the CASTOR 30B... configuration to accommodate the longer CASTOR 30XL SRM. 8.15. Hydrazine Servicing... the HIF for integration. The CASTOR 30 second stage motor and...



Дата загрузки: 2016-10-31
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0.09/5
... CASTOR MOTOR SERIES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 CASTOR IVA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 CASTOR IVA-XL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 CASTOR IVB. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 CASTOR 30. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 CASTOR 30B. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .28 CASTOR 30XL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 CASTOR 120. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 CASTOR 120XL... Space Propulsion Product portfolio: Orion, CASTOR®, CASTOR 120®, LCS (large class stage... of Orbital ATK, Inc. CASTOR® and CASTOR 120® are registered trademarks of... April 2016 200 CASTOR 30 200 300 300 CASTOR 120 LCS I 400... 92.1 Vectorable Vectorable Vectorable CASTOR 30XL CASTOR 120 Approved for Public Release... 92 92 Vectorable CASTOR 30B 40.1 40.1 CASTOR 30 Fixed Vectorable CASTOR IVA-XL 40.1 50.2 50.2 50.2 50.2 50.2 50.2 CASTOR IVB Fixed CASTOR IVA CASTOR Motor Family Fixed Vectorable... XL CASTOR 30XL CASTOR 120 2 1 0 1 Conventional Strike/Family of Motors Antares CASTOR 30B 1 4 LCS III Antares/Athena Ic/Athena IIc CASTOR 30 1 HII-A CASTOR IVA-XL 4 7 0 Maxus/Targets CASTOR IVB Conventional Strike/Family of Motors Delta II/Atlas 2AS CASTOR IVA 0 LCS I Taurus XL Orion 50S XLT 5 1 0 1 1 0 1 1 3 1 CASTOR 120XL... Catalog CASTOR® MOTOR SERIES LOW-COST, HIGH-RELIABILITY BOOSTERS The CASTOR motor... CASTOR IVA, IVA-XL, and IVB have replaced the CASTOR IV motor. • CASTOR IVA, high-performance strap-on propulsion launch vehicles • CASTOR... launches carry commercial satellites and CASTOR motors are designed to provide... CASTOR series. Development of the CASTOR 120 motor began in 1989. The CASTOR... CASTOR 30/30B and CASTOR 30XL have been added to the series. CASTOR 30/30B... Burnout...............................................................3,239 FIXED NOZZLE The CASTOR IVA motor was developed in... STATUS ........... FLIGHT PROVEN, INACTIVE PRODUCTION CASTOR® IVA Vaccum Thrust vs. Time... The CASTOR IVA-XL motor, an 8-foot extension of the CASTOR IVA... STATUS ........... FLIGHT PROVEN, INACTIVE PRODUCTION CASTOR® IVA-XL Vaccum Thrust vs... The CASTOR IVB motor was the first in the series of CASTOR... STATUS............................ ........... FLIGHT PROVEN, INACTIVE PRODUCTION CASTOR® IVB Vaccum Thrust vs. Time...°-105°F PRODUCTION STATUS........... FLIGHT-PROVEN CASTOR® 30 Vaccum Thrust vs. Time...; Dated 05 April 2016 27 CASTOR 30B MOTOR DIMENSIONS Motor diameter, in...-LINE UPPER STAGE BOOSTER The CASTOR 30B is a low cost, robust, state... incorporates a few modifications from the CASTOR 30, primarily a change in propellant...°-105°F PRODUCTION STATUS........... FLIGHT-PROVEN CASTOR® 30B Vaccum Thrust vs. Time 100000... motor. CASTOR 30XL is more than a stretched version of the CASTOR 30.... CASTOR 120XL is more than just a stretched version of the CASTOR 120... component development and qualification supporting CASTOR 30 motors. Motor diameter, in... component development and qualification supporting CASTOR 30 motors. Motor diameter, in... booster destruct applications on STAR, CASTOR, Titan, Atlas, and Delta • Semiconductor...



Дата загрузки: 2017-11-08
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0.06/5
FACT SHEET QUICK FACTS: Antares TM Medium-class space launch vehicle utilizes proven systems from other Orbital product lines and Zenit heritage Medium-Class Space Launch Vehicle Over 5,000 kg to low-Earth orbit Designed to achieve a 95% or greater launch reliability Key Partners: Orbital Sciences Corporation • Prime integrator, systems engineering, avionics, primary structure, testing and software • Overall Stage 1 development and integration KB Yuzhnoye/Yuzhmash • Stage 1 core design, production and verification Antares will launch from the newly built Pad-0A at Wallops Flight Facility, Virginia Overview Designed to provide responsive, low-cost, and reliable access to space, Antares is a twostage vehicle (with optional third stage) that provides low-Earth orbit (LEO) launch capability for payloads weighing over 5,000 kg. Internally funded by Orbital, Antares is currently under development with a total of 10 missions planned between 2012 and 2015: a risk reduction mission, a demonstration of commercial re-supply services for the International Space Station (ISS) under a NASA Commercial Orbital Transportation Services (COTS) agreement, and eight Commercial Resupply Missions (CRS) to deliver cargo to the ISS. The Antares launch system utilizes Orbital's proven MACH avionics system and many management approaches, engineering standards, production and test processes common to Orbital’s family of highly successful small-class Pegasus®, Taurus®, and Minotaur launch vehicles. These proven launch technologies, along with hardware from one of the world’s leading launch vehicle integrators, combine to provide cost-effective access to a variety of orbits for civil, commercial and military medium-class payloads. Aerojet • Stage 1 engines ATK • Stage 2 motor Antares is designed to achieve a 95% or greater launch reliability. Design, manufacturing and testing of Antares is taking place in Dulles, Virginia and Chandler, Arizona. Key Features • Incorporates both solid and liquid stages and flight-proven technologies to meet mediumclass mission requirements • Provides substantial payload performance into a variety of low inclination low-Earth and sun-synchronous orbits and interplanetary trajectories • Streamlined vehicle/payload integration and testing via simplified interfaces reduce time from encapsulation to lift-off • 3.9 meter fairing accommodates large payloads • Capable of launching single and multiple payloads • Initial launch capability in 2012 from Wallops Flight Facility (WFF), Virginia • Also compatible with the Western Range at Vandenberg Air Force Base (VAFB), Eastern Range at Cape Canaveral Air Force Station (CCAFS) and the Kodiak Launch Complex (KLC) Artist's rendering of Orbital's Antares mediumclass space launch vehicle GALEX Specs & Features Antares Expanded View Performance Circular Low-Earth Orbit Performance Payload Fairing • Diameter: 3.9 meters 8,000 7,000 • Structure: Honeycomb core, composite face 6,000 • Separation: Non-contaminating frangible ring Optional STAR™ 48-Based Third Stage • ATK STAR 48BV high energy upper stage solid rocket motor Stage 2 • ATK CASTOR ® 30B solid motor (CASTOR 120 heritage) with thrust vectoring • Thrust vector guidance and control • MACH avionics Payload Capability (kg) • Height: 9.9 meters Antares 130 Antares 121 28.7˚ 51.6˚ Sun Sync 28.7˚ 51.6˚ Sun-Sync 28.7˚ 51.6˚ Sun-Sync Antares 131 28.7˚ 51.6˚ Sun Sync 5,000 4,000 3,000 2,000 1,000 200 300 400 500 600 700 Circular Orbit Altitude (km) 800 900 1000 High Energy Performance • 3-axis stabilized satellite orbit insertion Optional Stage 2 • ATK CASTOR 30XL solid motor with thrust vectoring Legend Antares 120 2,000 Legend Antares 122 1,800 Antares 132 1,600 Payload Capability (kg) 1,400 Optional Bi-Propellant Third Stage (BTS) Helium pressure regulated bi-propellant propulsion system using nitrogen tetroxide and hydrazine (Orbital GEOStar™ bus heritage) 1,200 1,000 800 600 400 200 0 -10 -5 0 5 10 15 Earth Escape Energy (km2/s2) 20 25 Antares Configuration Numbering Stage 1 • Two Aerojet AJ26-62 engines with independent thrust vectoring First Stage Second Stage 1–Two AJ26-62 LOX/Kerosene Fueled Engines 2–CASTOR 30B 0–None Solid Motor 1–Bi-Propellant 3–CASTOR 30XL Third Stage (BTS) Solid Motor 2–STAR 48 Solid Motor • Liquid oxygen/kerosene fueled • Orbital responsible for system development and integration • Core tank design and design verification by KB Yuzhnoye (Zenit-derived) • Core tank production by Yuzhmash • Avionics stage controller uses flight-proven Orbital MACH components Third Stage Key Contacts Mark Pieczynski, VP Southern California Engineering Center and Space Launch Business Development 714/677-2444, pieczynski.mark@orbital.com Warren Frick, Program Manager Advanced Projects 703/948-8192, frick.warren@orbital.com Orbital Sciences Corporation | 45101 Warp Drive | Dulles, Virginia 20166 | www.orbital.com ©2012 Orbital Sciences Corporation. FS007_06L



Дата загрузки: 2017-05-21
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0.03/5
... different second stages, the Castor-30XL or the Castor-30B, both from Alliant... 3rd Stage Option Stage designation N/A Castor-30B/30XL STAR-48V Length, m (ft... Third Stage (BTS) 25 (82) 30B: 4.17 (13.7) 30XL: 5.99 (19... Solid 240,000 (529,109) 30B: 12,887 (28,411) 30XL... Stage Option 4th Stage Option Castor-120 Orion-50SXLG Orion-50XL... the ITU Radio Regulations (Appendix 30B), these smaller countries can gain...



Дата загрузки: 2017-10-09
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0.05/5
... 1st stage: Castor 120 solid motor 2nd stage: Castor 120 solid motor Orbit Adjust Module 3rd Stage: Castor 30 solid motor 1st stage: 2-Castor 120 solid motors 2nd stage Castor 120 solid motor Orbit Adjust Module 3rd Stage: Castor 30 solid motor 1st stage: 8 Castor 120 solid motors... 38 Taurus Taurus II 0 stage: Castor 120 1st stage Orion 50S... Titan IIc 2nd stage: ATK Castor-30B SRM 2nd stage (optional): High...-propellant stages. Stage 0 utilizes a Thiokol Castor-120 motor. The Taurus standard... propellants; the second stage is a Castor-30 SRM propelled by HTPB... and IIc use an ATK CASTOR 120 solid rocket motor (SRM... the Athena IIc uses a second Castor 120 for the second stage... a newly-developed and ground-tested CASTOR 30 SRM for their upper... of hydrazine, is available. Each Castor 120 motor contains 48,596... solid rocket propellant (SRP). The Castor 30 motor contains 12,814... designed to support up to Castor 120 boosted launch vehicles, including...-stage (Minotaur) rockets and commercial Castor IV class boosters, such as.... The expected launch noise from a Castor-120TM motor on the Athena... 10 ppm 146 μg/m3 8 ppm a. Castor 120 motor. Key: μg/m3=micrograms...



Дата загрузки: 2017-02-23
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0.03/5
Antares™ Medium-Class Space Launch Vehicle LAUNCH VEHICLE Medium Class FACTS AT A GLANCE Overview Designed to provide responsive and low-cost access to space, Antares is a two-stage vehicle (with optional third stage) that provides low-Earth orbit (LEO) launch capability for payloads weighing over 7,000 kg. Internally funded by Orbital, Antares completed a risk reduction mission and a demonstration of commercial re-supply services for the International Space Station (ISS) under a NASA Commercial Orbital Transportation Services (COTS) agreement in 2013. Orbital commenced delivery of cargo to the International Space Station under the NASA Commercial Resupply Services (CRS) contract in 2014. The Antares launch system utilizes Orbital's proven MACH avionics system and many management approaches, engineering standards, production and test processes common to Orbital’s family of successful small-class Pegasus® and Minotaur launch vehicles. The Antares design is being upgraded with newly-built RD-181 first stage engines to provide greater payload performance and increased reliability. Orbital is modifying the rocket’s first stage systems in anticipation of hot fire testing in late 2015. The company is currently targeting a return to flight in 2016 with launches projected in the first, second and fourth quarters to fulfill the company’s agreement with NASA to deliver supplies to the International Space Station. Key Features • Capable of launching single and multiple payloads • Provides substantial payload performance into a variety of low inclination low-Earth and sun-synchronous orbits and interplanetary trajectories • Initial launch capability from Wallops Flight Facility (WFF), Virginia • 3.9 meter fairing accommodates large payloads Over 7,000 kg to low-Earth orbit Mission Partners Orbital Sciences Corporation Prime integrator, systems engineering, avionics, primary structure, testing and software. Overall Stage 1 development and integration. KB Yuzhnoye/Yuzhmash Stage 1 core design, production and verification Energomash • Incorporates both solid and liquid stages and flight-proven technologies • Streamlined vehicle/payload integration and testing via simplified interfaces reduce time from encapsulation to lift-off Medium-class space launch vehicle utilizes systems from other Orbital product lines and Zenit heritage • Also compatible with the Western Range at Vandenberg Air Force Base (VAFB), Eastern Range at Cape Canaveral Air Force Station (CCAFS) and the Kodiak Launch Complex (KLC) Stage 1 engines ATK Stage 2 motor Antares ™ Expanded View Performance Payload Fairing Antares Performance to Circular Orbits (WFF) • Diameter: 3.9 m 7000 • Height: 9.9 m Antares Performance to Circular Orbits (WFF) 231 • Separation: Non-contaminating frangible ring Optional STAR™ 48-Based Third Stage Stage 2 Payload Mass (kg) 6000 • Structure: Honeycomb core, composite face Optional BiPropellant Third Stage (BTS) Optional Stage 2 • ATK CASTOR 30XL solid motor with Helium pressure regulated bi-propellant propulsion system using nitrogen tetroxide and hydrazine (Orbital GEOStar™ bus heritage) thrust vectoring • Thrust vector guidance and control 4000 3000 1000 100 300 400 500 600 700 Circular Orbit Altitude (km) 800 900 o 5000 • 3-axis stabilized satellite orbit insertion Antares Performance to 38 High Energy Orbits (WFF) 4500 4000 3500 3000 232 2500 2000 Stage 1 1500 • Two NPO Energomash RD-181 engines with independent thrust vectoring 1000 • Liquid oxygen/kerosene fueled 200 Antares Performance to 38˚ High Energy Orbits (WFF) Payload Mass (kg) • MACH avionics 230 5000 2000 • ATK STAR 48BV high energy upper stage solid rocket motor • ATK CASTOR® 30B solid motor (CASTOR 120 heritage) with thrust vectoring 38o 51.6o 60o 500 −50 −40 −30 −20 −10 0 2 2 C3 Energy (km /s ) 10 20 30 • Orbital responsible for system development and integration • Core tank design and design verification by KB Yuzhnoye (Zenit-derived) • Core tank production by Yuzhmash • Avionics stage controller uses flight-proven Orbital MACH components Key Contacts Mark Pieczynski VP Southern California Engineering Center and Space Launch Business Development (714) 677-2444 pieczynski.mark@orbital.com Warren Frick Program Manager Advanced Projects (703) 948-8192 frick.warren@orbital.com Orbital Sciences Corporation 45101 Warp Drive • Dulles, Virginia 20166 ©2014 Orbital Sciences Corporation FS007_06_3891 • www.orbital.com Antares Configuration Numbering First Stage Second Stage Third Stage 2 – Two NPO Energomash RD-181 Lox/ Kerosene Fueled Engines 2 – CASTOR 30B Solid Motor 0 – None 3 – CASTOR 30XL Solid Motor 1 – Bi-Propellant Third Stage (BTS) 2 – Star 48-Based Third Stage



Дата загрузки: 2017-03-18
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0.16/5
... flights with a CASTOR 30B second stage motor instead of the CASTOR 30 used... second stage consists of the CASTOR® 30B solid rocket motor, an avionics...



Дата загрузки: 2016-11-29
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0.05/5
Antares™ Medium-Class Space Launch Vehicle FACT SHEET Overview Designed to provide responsive and low-cost access to space, Antares is a two-stage vehicle (with optional third stage) that provides low-Earth orbit (LEO) launch capability for payloads weighing over 7,000 kg. Internally funded by Orbital ATK, Antares completed a risk reduction mission and a demonstration of commercial re-supply services for the International Space Station (ISS) under a NASA Commercial Orbital Transportation Services (COTS) agreement in 2013. Orbital ATK commenced delivery of cargo to the International Space Station under the NASA Commercial Resupply Services (CRS) contract in 2014. The Antares launch system utilizes Orbital ATK's proven MACH avionics system and many management approaches, engineering standards, production and test processes common to Orbital ATK’s family of successful small-class Pegasus® and Minotaur launch vehicles. The Antares design is being upgraded with newly-built RD-181 first stage engines to provide greater payload performance and increased reliability. Orbital ATK is modifying the rocket’s first stage systems in anticipation of hot fire testing in second quarter 2016. The company is currently targeting a return to flight in third quarter 2016 with a second launch projected in the fourth quarter to fulfill the company’s agreement with NASA to deliver supplies to the ISS. Orbital ATK was also recently awarded a CRS-2 contract for cargo deliveries through 2024. • Incorporates both solid and liquid stages and flight-proven technologies • 3.9 meter fairing accommodates large payloads • rovides substantial payload performance P into a variety of low inclination lowEarth and sun-synchronous orbits and interplanetary trajectories • apable of launching single and multiple C payloads • Launch capability from Wallops Flight Facility (WFF), Virginia Streamlined vehicle/payload integration and testing via simplified interfaces reduce time from encapsulation to lift-off Medium-class space launch vehicle utilizes systems from other Orbital ATK product lines and Zenit heritage Over 7,000 kg to low-Earth orbit Mission Partners Orbital ATK Prime integrator, systems engineering, avionics, primary structure, testing and software. Overall Stage 1 development and integration KB Yuzhnoye/Yuzhmash Stage 1 core design, production and verification Key Features • FAC T S AT A G L A N C E NPO Energomash Stage 1 engines Orbital ATK Stage 2 motor ™ Expanded View Performance Payload Fairing Antares Performance to Circular Orbits (WFF) • Diameter: 3.9 m 7500 7000 • Height: 9.9 m 6000 • Structure: Honeycomb core, composite face Stage 2 • Orbital ATK CASTOR ® 30XL solid motor (CASTOR 120 heritage) with thrust vectoring • Orbital ATK STAR 48BV high energy upper stage solid rocket motor • MACH avionics Optional BiPropellant Third Stage (BTS) Optional Stage 2 • Orbital ATK CASTOR ® 30B solid motor with thrust vectoring Helium pressure regulated bi-propellant propulsion system using nitrogen tetroxide and hydrazine (Orbital ATK GEOStar™ bus heritage) • Thrust vector guidance and control Payload (kg) Optional STAR™ 48-Based Third Stage SSOº 231 5500 • Separation: Non-contaminating frangible ring %& '($) )* 38º 51.6º 230 6500 5000 4500 4000 3500 3000 2500 2000 1500 1000 500 0 0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 Circular Orbit Altitude (km) Antares Performance to 38˚ High Energy Orbits (WFF) o 5000 • 3-axis stabilized satellite orbit insertion Antares Performance to 38 High Energy Orbits (WFF) 4500 4000 Payload Mass (kg) Antares 3500 3000 232 2500 2000 1500 Stage 1 1000 • Two NPO Energomash RD-181 engines with independent thrust vectoring 500 −50 • Liquid oxygen/kerosene fueled −40 −30 −20 −10 0 C3 Energy (km2/s2) 10 20 30 • Orbital ATK responsible for system development and integration • Core tank design and design verification by KB Yuzhnoye (Zenit-derived) Antares Configuration Numbering • Core tank production by Yuzhmash • Avionics stage controller uses flight-proven Orbital ATK MACH components First Stage Second Stage Third Stage 2 – Two NPO Energomash RD-181 Lox/ Kerosene Fueled Engines 2 – CASTOR® 30B Solid Motor 0 – None 3 – CASTOR® 30XL Solid Motor 1 – Bi-Propellant Third Stage (BTS) 2 – STAR 48-Based Third Stage Key Contacts John Steinmeyer Director, Business Development Warren Frick Program Manager, Advanced Projects (714) 677-2440 john.steinmeyer@orbitalatk.com (703) 948-8192 warren.frick@orbitalatk.com OrbitalATK.com ©2015 Orbital ATK, Inc. All Rights Reserved. FS007_06_OA_3695



Дата загрузки: 2017-11-08
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COTS/CRS Commercial Resupply Services for the ISS INNOVATION YOU CAN COUNT ON ® COTS/CRS INTRODUCTION & SYSTEM OVERVIEW Under a Commercial Orbital Transportation Services With the award of the Commercial Resupply Service (COTS) cooperative agreement, Orbital and NASA are (CRS) contract, NASA selected Orbital to provide eight jointly developing a new space transportation system pressurized cargo missions beginning in 2012 and running to demonstrate the capability to provide cargo delivery through 2015. For NASA, CRS will provide a U.S.-produced services to the International Space Station (ISS). The COTS and-operated automated cargo delivery service for ISS program will involve full-scale development and a 2012 flight logistic support, to complement Russian, European and demonstration of a commercial cargo delivery system, and Japanese ISS cargo vehicles. consists of two elements: • The Antares™ medium-class space launch vehicle • The Cygnus™ advanced maneuvering spacecraft, which includes a pressurized cargo module developed by Orbital and its industrial partner Thales Alenia Space Much of the development of the Orbital COTS/CRS system is internally funded. Industrial partners include some of the world’s leading space companies providing heritage subsystems with flight-proven heritage to ensure high reliability. To support the COTS/CRS missions, new ground support and launch facilities are being built at NASA’s Wallops Flight Facility, Virginia. ANTARES SPACE LAUNCH VEHICLE Antares is a two-stage launch vehicle designed to provide responsive, cost-effective, and reliable access to orbit and Earth escape for medium-class payloads weighing over 5,000 kg. Antares is designed to be a highly-reliable launcher to meet NASA Category 3 and similar DoD mission success standards, and incorporates flight-proven subsystems to reduce development cost, schedule and risk. SYSTEM FEATURES • Incorporates both solid and liquid stages and flight-proven technologies to meet medium-class mission requirements • Provides substantial payload performance into a variety of low inclination low-Earth and sun-synchronous orbits and interplanetary trajectories Launch Vehicle • Diameter: 3.9 meters • 3.9 meter fairing accommodates large payloads • Height: 40.0 meters • Streamlined vehicle/payload integration and testing via simplified avionics interfaces reduces time from encapsulation to lift-off • Mass: 290,000 kg • Initial launch capability in 2012 from Wallops Flight Facility (WFF) Stage 2 • ATK CASTOR® 30B/30XL solid motor (CASTOR 120 heritage) with thrust vectoring • Capable of launching single and multiple payloads • Compatible with the Western Range at Vandenberg Air Force Base (VAFB), Eastern Range at Cape Canaveral Air Force Station (CCAFS) and Kodiak Launch Complex (KLC) • Avionics using Orbital MACH components Stage 1 • Two Aerojet AJ26-62 engines each with independent thrust vectoring • Liquid oxygen/kerosene fueled • Orbital responsible for system development and integration • Core tank assembly design and design verification by KB Yuzhnoye (Zenit-derived heritage) • Core tank assembly production by Yuzhmash • Stage controller using flight-proven Orbital MACH components ORBITAL SCIENCES CORPORATION FOR MORE INFORMATION: 21839 Atlantic Boulevard, Dulles, VA 20166 703/406-5000 www.orbital.com Mr. Frank DeMauro, VP and Program Director COTS/CRS Program 703/948-8766, demauro.frank@orbital.com Mr. Carl Walz, Deputy Program Manager COTS/CRS Program 703/404-7475, walz.carl@orbital.com CYGNUS ADVANCED MANEUVERING SPACECRAFT The Cygnus advanced maneuvering spacecraft is a low-risk design incorporating elements drawn from Orbital and its partners’ existing, flight-proven spacecraft technologies. Cygnus consists of a common service module and a pressurized cargo module. The service module incorporates avionics, propulsion and power systems from Orbital’s flight-proven GEOStar™ and LEOStar™ satellite lines. The pressurized cargo module is based the on the Multi-Purpose Logistics Module (MPLM), developed by Thales Alenia Space for NASA. The module will carry crew supplies, spares and scientific experiments. Service Module (SM) • Design, integration and test performed by Orbital • Heritage: GEOStar, LEOStar • Gross Mass: 1,800 kg • Power Generation: 2 fixed wing solar arrays, ZTJ Gallium Arsenide cells • Power Output: 3.5 kW (sun-pointed) • Propellant: Dual-mode N2H4 /MON-3 or N2H4 Pressurized Cargo Module (PCM) • Design, integration and test performed by Thales Alenia Space • Heritage: Multi-Purpose Logistics Module • Gross Mass: 3,500 kg • Total Cargo Mass: 2,000 kg Standard / 2,700 kg Enhanced • Pressurized Volume: 18.9 m3 / 27 m3 • Berthing at ISS: Node 2 Common Berthing Mechanism (CBM) ©2011 Orbital Sciences Corporation G008_09f