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Shaviyt 1
Part of Jericho
Israeli all-solid orbital launch vehicle. Shavit 1 is an improved version of the original Shavit with a stretched first stage motor.
AKA: NEXT;Shavit 1. Status: Active. First Launch: 1995-04-05. Last Launch: 2014-04-09. Number: 7 . Payload: 225 kg (496 lb). Thrust: 760.00 kN (170,850 lbf). Gross mass: 30,000 kg (66,000 lb). Height: 18.00 m (59.00 ft). Diameter: 1.35 m (4.42 ft). Apogee: 366 km (227 mi).
LEO Payload: 225 kg (496 lb) to a 366 km orbit at 143.00 degrees. Launch Price $: 15.000 million in 1999 dollars.
Stage Data - Shavit 1
- Stage 1. 1 x LK-1. Gross Mass: 13,990 kg (30,840 lb). Empty Mass: 1,240 kg (2,730 lb). Thrust (vac): 774.000 kN (174,002 lbf). Isp: 268 sec. Burn time: 55 sec. Isp(sl): 250 sec. Diameter: 1.35 m (4.42 ft). Span: 1.50 m (4.90 ft). Length: 7.50 m (24.60 ft). Propellants: Solid. No Engines: 1. Engine: LK-1. Status: Development 2002. Comments: Lengthened version of Shavit/RSA-3 rocket motor. For lower stage use with 17.1:1 nozzle. Fitted with 23.6:1 nozzle for upper stage use specific impulse increases to 279 seconds, length to 8.4 m, and empty and gross mass are increased by 135 kg.
- Stage 2. 1 x RSA-3-2. Gross Mass: 10,971 kg (24,186 lb). Empty Mass: 1,771 kg (3,904 lb). Thrust (vac): 476.600 kN (107,144 lbf). Isp: 277 sec. Burn time: 52 sec. Isp(sl): 220 sec. Diameter: 1.30 m (4.20 ft). Span: 1.30 m (4.20 ft). Length: 6.40 m (20.90 ft). Propellants: Solid. No Engines: 1. Engine: RSA-3-2. Status: Out of production. Comments: Source: Missile exhibit and placards, AF Museum, South Africa. Empty mass includes 583 kg for payload shroud, guidance, orientation and spin-up platform that positions stage 3 and payload for final orbital insertion burn.
- Stage 3. 1 x RSA-3-3. Gross Mass: 2,048 kg (4,515 lb). Empty Mass: 170 kg (370 lb). Thrust (vac): 58.800 kN (13,219 lbf). Isp: 298 sec. Burn time: 94 sec. Diameter: 1.30 m (4.20 ft). Span: 1.30 m (4.20 ft). Length: 2.60 m (8.50 ft). Propellants: Solid. No Engines: 1. Engine: RSA-3-3. Status: Out of Production. Comments: Data accurate. Source: Missile exhibit and placards, AF Museum, South Africa. ARC/Rafael AUS 51 is identical.
More at: Shaviyt 1.
Family:
all-solid,
orbital launch vehicle.
Country:
Israel.
Spacecraft:
Ofeq 3,
Ofeq 5,
Tecsar.
Projects:
Ofeq.
Launch Sites:
Palmachim.
Stages:
LK-1 engine,
RSA-3-2,
RSA-3-3.
Agency:
IAI.
1995 April 5 - .
11:16 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-3 - .
Mass: 189 kg (416 lb). Nation: Israel.
Agency: ISA.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 3.
Decay Date: 2000-10-24 . USAF Sat Cat: 23549 . COSPAR: 1995-018A. Apogee: 694 km (431 mi). Perigee: 366 km (227 mi). Inclination: 143.40 deg. Period: 94.50 min.
1998 January 22 - .
12:56 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
FAILURE: Launch vehicle failed during second stage burn..
Failed Stage: 2.
- Ofeq-4 - .
Mass: 189 kg (416 lb). Nation: Israel.
Agency: ISA.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 3.
Fell in Mediterranean Sea..
2002 May 28 - .
15:25 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-5 - .
Mass: 300 kg (660 lb). Nation: Israel.
Agency: Tsahal.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
USAF Sat Cat: 27434 . COSPAR: 2002-025A. Apogee: 757 km (470 mi). Perigee: 370 km (220 mi). Inclination: 143.50 deg. Period: 95.90 min.
Military Observation satellite. Return to flight of the Shavit booster following a lauanch failure. Launch delayed from third quarter 2001. The three-stage Shavit rocket took off from Palmachim Air Force Base on the Israeli coast and flew westward to put the satellite in a retrograde orbit. The AUS-51 third stage solid motor entered a 262 x 774 km x 143.5 deg orbit and separated from the Ofeq satellite. Both coasted up to apogee at around 1620 UTC when Ofeq made a burn to increase its velocity by 33 m/s, raising the orbit to 369 x 771 km x 143.5 deg.
2004 September 6 - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
FAILURE: Third stage orientation failure at 270 seconds into the flight.
Failed Stage: 3.
- Ofeq-6 - .
Mass: 300 kg (660 lb). Nation: Israel.
Agency: Tsahal.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
Military observation satellite failed to reach orbit. Finanical loss estimated by Israeli press as $ 100 million..
2007 June 10 - .
23:40 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-7 - .
Mass: 300 kg (660 lb). Nation: Israel.
Agency: Tsahal.
Manufacturer: IAI.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
USAF Sat Cat: 31601 . COSPAR: 2007-025A. Apogee: 576 km (357 mi). Perigee: 340 km (210 mi). Inclination: 141.80 deg. Period: 93.80 min. Israeli optical reconnaisance satellite, evidently using an improved version of the Shavit booster and probably heavier and more capable than its predecessors..
2010 June 22 - .
19:00 GMT - .
Launch Site:
Palmachim.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq 9 - .
Mass: 189 kg (416 lb). Nation: Israel.
Agency: ISA.
Program: Ofeq.
Class: Surveillance.
Type: Military surveillance satellite. Spacecraft: Ofeq 5.
USAF Sat Cat: 36608 . COSPAR: 2010-031A. Apogee: 586 km (364 mi). Perigee: 400 km (240 mi). Inclination: 141.80 deg. Period: 94.50 min. Israeli optical surveillance satellite..
2014 April 9 - .
19:06 GMT - .
Launch Site:
Palmachim.
Launch Pad: xxx.
LV Family:
Jericho.
Launch Vehicle:
Shaviyt 1.
- Ofeq-10 - .
Mass: 260 kg (570 lb). Nation: Israel.
Class: Surveillance.
Type: Military Radarsat. Spacecraft: Tecsar.
USAF Sat Cat: 39650 . COSPAR: 2014-019A. Apogee: 598 km (371 mi). Perigee: 388 km (241 mi). Inclination: 140.94 deg. Period: 94.48 min. Reportedly carried a radar imaging (SAR) payload..
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