lux.gif

's type collection


print view : pr_print.gif

Today: 14. Dec 17, visitors total: 3143

please select the headline:

ZENIT-J1 launch vehicle


ZENIT-J1
US DoD: SL-16

* Developer:
NPO Yuzhnoye (Ukraine)
* Payload:
- 13,740 kg to 200 km Orbit
-   5,180 kg to Geosynchronous transfer trajectory

Faring

* Chronology:
- First Launch Date : 04/13/1984
- Last Launch Date : 10/31/1995
- Launches
    Total Number: 30
    Number of Failure: 4
- Success Rate : 86.67 %
* Launch Vehicle:
- Total Mass: 461,900 kg
- Liftoff Thrust: 769,880 kgf
- Length with Faring: 57.00 m
- Core Diameter: 3.90 m

Zenit-J1

ZENIT J1

* Stage 3:
- Engine: RD-58 11D58D
- Number of Engines: 1
- Total Thrust (vac): 7,240 kgf
- Specific Impulse: 361 sec
- Burn Time: 660 sec
- Gross Mass: 17,300 kg
- Empty Mass: 3,100 kg
- Propellants: Kerosene / LOX
- Length: 5.50 m
- Length Faring: 13.65 m
- Core Diameter: 3.70 m

Stage 3 without Faring

* Stage 2:
- Engine: RD-120 11D123
- Number of Engines: 1
- Total Thrust (vac): 93,000 kgf
- Specific Impulse: 349 sec
- Burn Time: 315 sec
- Gross Mass: 90,400 kg
- Empty Mass: 8,400 kg
- Propellants: Kerosene / LOX
- Length: 11.50 m
- Core Diameter: 3.90 m

Stage 2

* Stage 1:
- Engine: RD-171 11D520
- Number of Engines: 4
- Total Thrust (vac): 834,243 kgf
- Specific Impulse: 337 sec
- Burn Time: 150 sec
- Gross Mass: 354,200 kg
- Empty Mass: 27,900 kg
- Propellants: Kerosene / LOX
- Length: 32.06 m
- Core Diameter: 3.90 m

Stage 1

/ back to the top of ZENIT-J1 launch vehicle /


Artworks:

ZENIT-J1 launch vehicle    

cd61-0060ze
ZENIT launch vehicles
    => enlarge
    CDes# cd61-0060ze => order now

Lux's type collection of ZENIT-J1 launch vehicle
 
my sitemap back to my mainsite e-mail me search through my homepage   

Powered by
the Fluid Dynamics Search Engine
v2.0.0.0073 © 2005

  CopyInfo for homepage 1997-2017 by B.Lux, Hamburg - Germany
                    and David Metreveli - Israel.