Ракетный блок. KM-V2b. [Редактировать]

Технические характеристики

#ХарактеристикаЗначение
1Длина, метра2.3
2Тяга (пустота), кНьютон99.8
3Удельный импульс, сек300
4Масса, кг3300
5Масса (корпуса), кг800
6Масса (топлива), кг2500
7Диаметр, метра1.4
8Типтвердотопливный

Найдено 27 документов по запросу «KM-V2b». [Перейти к поиску]


Дата загрузки: 2017-05-21
Скачать документ
Скачать текст
0.04/5
... constitutes the second stage, and a KM-2Vb represents the third stage... Length, m (ft) SRB-A3 M-34c KM-V2b Post Boost Stage 15 (49... is a newly manufactured Khrunichev Breeze-KM upper stage. A payload adapter and... payload, it became the Rockot-KM, which has launched 21 times... Services for international customers. Rockot-KM currently has a backlog of commercial... 1st Stage 2nd Stage Breeze-KM 17.2 (56.4) 3.9 (12.8) 2.5 (8.2) 2.5 (8.2) 2.5 (8.2) 2.5 (8.2) OKB-52... orbits as high as 1,500 km (932 mi) in altitude. The... vehicles will also use Breeze-KM and Breeze-M upper stages. An..., m (ft) Mass, kg (lb) Apogee, km (mi) Flight duration 2013 Propellant..., vertical landing Seats Participants: 3 Apogee, km (mi) 100 (62) • 54 • SPACELOFT..., kg (lb) 36 (79) Apogee, km (mi) 160 (99) Time in..., kg (lb) 600 (1,323) Apogee, km (mi) 110 (68.4) Time in..., kg (lb) 10 (22) Apogee, km (mi) 30.5 (19) Flight Duration... Cargo Capacity, kg (lb) 0 Apogee, km (mi) 30 (18.6) Time in... in Denmark. Seats: 1 Altitude: 100 km (62 mi) Mass: ~300 kg... - Pilots: 2 - Passengers: ~8 Altitude: 115 – 150 km (71-93 mi) Payload: 1,200...) payloads to LEO. Seats: N/A Altitude: 4.6 km (2.9 mi) Mass: TBD Propulsion: LOX... a satellite. Seats: TBD Altitude: 80 km (50 mi) Mass: TBD Payload... altitude of between 450 km and 600 km. Because no technical details...



Дата загрузки: 2016-12-29
Скачать документ
Скачать текст
0.39/5
Epsilon Launch Vehicle The Epsilon Launch Vehicle is a solid propellant rocket suitable for a new age, delivering both high performance and low cost. Based on the M-V Launch Vehicle, a multistage solid propellant rocket with the best performance in the world (discontinued in 2006), we try to achieve improved performance with the Epsilon Launch Vehicle, and build a system which will allow the frequent launch of launch vehicles by largely-reducing operational costs through enhancing aspects of operational efficiency, such as assembly and inspection. Through increased launch opportunities, we anticipate that space development activity will increase. The biggest goal of the Epsilon Launch Vehicle is to make space more accessible as rocket launches are made easier. The First Step to Future Launch Vehicles Post Boost Stage Payload Compact Liquid Propulsion System Fairing Second Stage Avionics Third Stage KM-V2b Third Stage Solid Motor(KM-V2b) [Launch System Innovation] Conventional launch vehicles required a significant period of time and effort to launch. With the Epsilon Launch Vehicle, launch systems are improved and simplified in order to reduce time for launch preparation. This will make times to launch the shortest in the world. Notably, the inspection of on-board devices will be done autonomously by the launch vehicle itself, thus streamlining inspection on the ground. This advance will allow the launch control of launch vehicles to be done anywhere in the world, simply by connecting a laptop computer to the network. This means having an ultimate launch control system which is independent of launch sites. We believe that these innovative concepts are a world first, and will be a role model for future launch vehicles. Second Stage Avionics Second Stage M-34c Second Stage Solid Motor(M-34c) Reaction Control System System Checkout Test of Epsilon the first Epsilon Launch Vehicle First Stage SRB-A First Stage Solid Motor(SRB-A) Standard Configuration Optional Configuration Three-staged Solid Propellant Launch Vehicle Three-staged Solid Propellant Launch Vehicle Compact Liquid Propulsion System /Epsilon Specifications Length m 24 Mass ton 91 /Specifications /Launch Capacity LEO SSO 4-6 101-8008 Tel.03-5289-3650 Fax.03-3258-5051 Japan Aerospace Exploration Agency Public Affairs Department Ochanomizu sola city, 4-6 Kandasurugadai, Chiyoda-ku, Tokyo 101-8008, Japan Phone:+81-3-5289-3650 Fax:+81-3-3258-5051 1200kg 250km x 500km 700kg 500km circle − 450kg 500km circle JAXA Website http://www.jaxa.jp/ JAXA Mail Service http://www.jaxa.jp/pr/mail/ JSF130510



Дата загрузки: 2017-04-24
Скачать документ
Скачать текст
0.02/5
... stage 3rd-stage solid motor (KM-V2b) 2/3-stage joint 2nd-stage equipment... of up to 190 km, 350 km and 1000 km respectively. The S-310... atmosphere at a speed of 12 km/ s, protected from harsh temperatures by...



Дата загрузки: 2017-02-23
Скачать документ
Скачать текст
0.15/5
... (PBS) (Optional Stage) Third Stage (KM-V2b) Second Stage (M-35) First Stage... Conditions Item Alt-Apogee [km] Alt-Perigee [km] Inclination [deg] Result 954...



Дата загрузки: 2017-04-23
Скачать документ
Скачать текст
0/5
...’s range from 160 to 320 km Athlon has taken several steps... (Exhibit 1.4) – aiming for a 95 g CO2/km cap by 2020; and regulations..., a target of 68-78 g CO2/km was proposed for 2025, with... standards in select regions g CO2/km normalized to New European Driving... EU target of 130 g CO2/km effective as of 2012, with... EU proposal of 95 g CO2/km for 2020; 2025 initial proposal... must improve to 93 g CO2/km (59.1 mpg) in 2025 from the 152 g CO2/ km (36.2 mpg) threshold in 2016... in Europe (NEDC) in g CO2/km 148 141 1321 139 1442... vehicles emitting less than 75 g/km (Exhibit 1.6). Stimulating EV demand: Governments... vehicles emitting less than 75 g/km 6,500 0 6,500 6,022 0 5,976 0 6,022... in 2011, 300 vehicles (135 km range) Launched Autolib’ in 2011, 2,000 vehicles (250 km urban range) e-scooter sharing service... with Madrid, 23 vehicles (200 km range) e-scooter sharing service (2013... ECar club in 2013 (145200 km range) Launched Move About in... CO2 emission reduction to 40 g/km in 2050 – a scenario that foresees... CO2 emission reduction to 10 g/km in 2050, representing the global... emission reduction to 95 g CO2/km in 2050. This would imply... annual mileage of 20,000 km and a holding period of four... 100 Cap of 10 g CO2/km in 2050 Cap of 40 g CO2/km in 2050 100 90 90... KIP Cap of 95 g CO2/km in 2050 ICE (optimized) HEV... UK ESTONIA 400 km NETHERLAND 100 km GERMANY 300 km Estonia’s nationwide EV... 40 to 60 km between charging points. 150 km The fast-charging... purchase electric cars. FRANCE 400 km PORTUGAL SOURCE: CHAdeMO 2013; Estonia electromobility program (ELMO) 400 km SPAIN 400 km Chapter 3: Charging infrastructure A new... a nominal maximum range of 200 km, and the Tesla Model S with... a nominal maximum range of 426 km. This reduced range capacity compared... a BEV with a range of 150 km who has the opportunity to... driving distances average 40-80 km per day, with 2-3 trips per..., driving an EV 15,000 km per year and charging it... SOURCE: McKinsey Vehicle to Building (V2B). The storage capacity of the... 1-2 days. Nissan is piloting this V2B approach in Japan, with the...



Дата загрузки: 2017-01-16
Скачать документ
Скачать текст
0.22/5
...–0.15 <3 0:5 F ring 140,200 (W Š 50 km) 0.1–0.5 G ring E ring 166,000–173... near Enceladus a Distance units in km b Power law index of the... for ice (about 140,000 km from Saturn’s center, see Section... 1 m, and perhaps as large as 1 km) surrounded by dusty transient structures... Roche Limit (around 140,000 km, see Section 17.2.2) in the... 70,000 to 136,000 km from Saturn’s center, or about... system’s age (using r D 15; 000 km, 3 10 3 m2 =s < ž < 3 10 2 m2 =s). Conversely... Eq. (17.7) with r D 25; 000 km, £ D 3, c D 10 3 m=s (corresponding to a 10 m thick... Eq. (17.7), with r D 20; 000 km, ž D 2:7 10 5 m2 =s (from the Daisaka... impact speed larger than 30 km/s, the impact ejecta are thrown... events ranging from 27 m to 9 km in width (see Fig. 17... resolution. Pywacket, the event 10 km outside the F ring core, is... may be insufficient to achieve km-size objects (Albers and Spahn... imply the destruction of a 200 km radius moon (!). An alternate explanation... a matter of debate (see Charnoz 3 km=s and et al. 2009a). Levison...) give V1 find P 5:6 10 24 km 2 =year in the present-day... al. 2009). Assuming a Mimas 200 km) is present at 100,000... sized satellite (rs Saturn, a 20 km radius comet is necessary to... Disk with radii larger than 1 km is about 109 . Assuming a size... Nc .>r/ / r 2:5 , we get Nc .>20 km/ 5 105 . Using Eq. (17.9) with... progenitor located at 100,000 km from Saturn is about Ni... to suggest that a 200–300 km radius satellite was destroyed in... a Mimas-mass moon located 105 km from Saturn can be destroyed.... (2007) suggested that a big (300 km radius or more) “comet” or... of objects larger than 300 km is far too low, by... distance of the rings ( 27 km=s). As a result, a copious exchange of... of ejected material ( 102 –103 km) was generated near, and propagated.... Durisen concluded that the 100 km structures seen in the inner... over scales of 1,000–3,000 km which they assert are not... inner C Ring and about 8,000 km beyond the F Ring. So it... over 1=2 all impact angles) Vr D " V2b C V2e C 2rp 2=3 , with rp D .a C a0... velocity: " "crit D v2e C 2rp 2=3 9 v2e C v2b C 2rp 2=3 #1=2 (17.13) ©crit is... for ice at 138;000 km, in very good agreement with...’s outer edge at 136;800 km. Numerical simulations (Karjalainen and Salo... , which is less than 100 km for the ILRs of Prometheus... erosion and periodic destruction of km-sized moonlets due to meteoroid... for significantly large bodies ( 500 km). For example, the inner icy... disrupted only below 76,000 km from Saturn’s center (Saturn’s equatorial radius is about 60,300 km for comparison), well inside the... Tremaine (1982) suggest that a 100 km radius satellite can survive undisrupted at 100,000 km from Saturn’s center, well inside...). Assuming an impact velocity 34 km=s p ( 3 times the circular orbital velocity at 105 km; Lissauer et al. 1988, Zahnle... icy body with radius r D 200 km would require an icy impactor between 10 and 20 km radius (Charnoz et al. 2009... al. (2009) find that a 200 km radius satellite could expect about....2 and 17.3). In addition, a 200 km moon may contain a substantial fraction... case that a broken-up ( 200 km) moon may have been predominantly... that Chiron, which has v1 D 3 km=s with respect to Saturn, was... (1) Chiron has a mean radius r D 90 km; (2) Centaurs have internal densities of... Saturn is uniform between 0 and 6 km/s; (4) the cumulative size distribution N(r), i.e., the... to 250, 500, or 1,000 km. Dones estimated that, on average, Centaurs with r > 90 km pass through the “Roche zone... least) a Mimas-sized body (r D 200 km) with unit density, and at..., with a pre-disruption diameter of 1:5 km and a material density of 0:6 g=cm3... known whether Centaurs hundreds of km in size are rubble piles...). This narrow ring lies 3,400 km beyond the A Ring’s outer edge... eccentric ringlet, with about 2,000 km full radial width but radially... component (the “core”) about 20 km wide in Cassini ISS images.... 1992), which may hide within a 1-km wide inner core seen in... a population of extended (30 m to 1.5 km) bodies that could be either... al. 2008) reveal a wealth of km-scale dynamical structures that still... a vertical extent of about 21 km, thus implying an ongoing dynamical... estimate equivalent to a 15–70 km radius body, roughly the size... scattered over more than 1,000 km in only 160 years, implying that 20 km wide structures like the F Ring... number of bodies larger than 1 km diameter seems to be correctly... of an underlying population of 0.1– 1 km sized moonlets. They developed a detailed... moonlets spread over a region 2000 km wide collide and release surface... of an F Ring core only 1 km wide (recently confirmed by Murray... ring at high velocity ( 30 km=s), as in other dusty rings... origin of the population of km-sized moonlets. Cuzzi and Burns...’s brightness peaks around 168,000 km from Saturn’s center, over 15,000 km from the nearest known satellite... brightness enhancement at 167,500 km from Saturn’s center, near the... at half-maximum of 250 km and extends over only 60...



Дата загрузки: 2017-01-30
Скачать документ
Скачать текст
1.2/5
... являет­ ся медианой, значит, или KM+ME=EF+FC, КМ+а=х+а. Следовательно... теореме косинусов находим, что KMN = KM 2 +KN 2 -2KM·KNcos45o = ~с 2 + ~d 2 - ~cd../2 = = ~(c 2 +d 2 -cd... sin LA - mn+kn · ::~;~ +km· ::~;~ mn+kn · ~ +km· ~ = ------~~Ь~с----~~= ------Ь~с~--~= mna+knb+kmc аЬс.... Поскольку КА= КС и ML+LK+KM = BL =LC, то ML+(LC+CК)+KM = (ML+LC)+(CK+KM) = = (ML+LB)+(AK+KM) = =МВ+АМ... МВ= МА =АВ= а. Тогда ВК =а(~ -1), KM=aR r ' а т. к. LKBA = 120°, то по... основание треугольника. Ответ: .j2a(a+b) или V2b(a+b). Решение. Первый способ. Пусть окружность... =а, то аналогично получим, что ВС= V2b(a+b). 12.10. В окружности с центром О проведены...



Дата загрузки: 2017-02-06
Скачать документ
Скачать текст
0.95/5
... KM-1200 KM-1600 KM-2000E KM-2000U KM-2500E KM-2500U KM-3000E KM-3000U KM-5000 KM-BK5006 KM-C1U KM-D600 KM-E300 KM-F250(A) KM-F250B KM-F250E KM-F250U KM-V7EG KM-V7EK KM... PC-V1V PC-V2A PC-V2B PC-V2C PC-V2E PC... XL-V282BK XL-V284BK XL-V2B XL-V300 XL-V300B XL...



Дата загрузки: 2017-05-21
Скачать документ
Скачать текст
0.05/5
.../04/2009 GROUND SOLUTIONS LIMITED KM&R DEVELOPMENTS LTD/RIGBY'S 06081617 01...) LTD 03726848 (N) 07/04/2009 A + KM TRADING LIMITED AAG PRIVATE CLIENTS LIMITED 05390261 (N) 05/04/2009 A + KM TRADING LIMITED AAG PRIVATE CLIENTS... & BUILD LIMITED 5K FOUNDATION LIMITED 5 KM LTD. FIVE LAMPS WINE BAR...) LIMITED K L TECHNOLOGIES LIMITED K- MAX LTD KM BAUMANAGEMENT LTD. K M BUILDERS & GROUNDWORKS LTD KM BUTCHERS & GROCERS LIMITED K MCKENZIE LTD K M ... LIMITED KM PARTNERS LIMITED KM PROJECT SERVICES LIMITED KM RADIO LIMITED KM RADIO LIMITED... SECRETARIES LIMITED KMT PUBLISHING LTD KM TV LIMITED KM2 ADVERTISING & DESIGN... UNITED KINGDOM LTD VTT LIMITED V2B COMMUNICATIONS LIMITED V2 MATRIX LIMITED...



Дата загрузки: 2017-05-20
Скачать документ
Скачать текст
1.25/5
... an altitude of 20,000 Km and have a mean velocity of 14,000 km/hr. Special relativity implies that... Space Station (ISS; height 400 Km, rotation period 90 min, inclination... (t B ) riB(G) + Bij (t B ) riB(G) r B(G) + C (tb , x B ) + O(c−5 ) = c4 v2B(G) tB 1 + w Bext ( x B(G) ) + viB(G) riB(G) + O(c−4 ), dt...., v B(G) = |v B(G) |, β B(G) = v B(G) /C, γB(G) = (1 − β2B(G) )−1/2 ) t G = γB( G ) t B − v B( G ) · x B c2 x G = x B − γB( G ) v B( G ) t B + www.intechopen.com + O ( c −4 ), γB( G ) − 1 v2B(G) v B ( G ) · x B v B ( G ) + O ( c −4 ). Relativistic Metrology: From Earth to...