CZ-1M-3
Gross Mass
: 1,830 kg (4,030 lb).
Empty Mass
: 256 kg (564 lb).
Thrust (vac)
: 29.400 kN (6,609 lbf).
Isp
: 291 sec.
Burn time
: 150 sec.
Propellants
:
Solid
.
Isp(sl)
: 115 sec.
Diameter
: 1.30 m (4.20 ft).
Span
: 1.30 m (4.20 ft).
Length
: 2.30 m (7.50 ft).
Country
:
China
.
No Engines
: 1.
Engine
:
Iris
.
Status
: Out of production.
Cost $
: 0.300 million.
First Flight
: 1991.
Used on Launch Vehicles:
CZ-1M
.
Contact us
with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site.
.
To contact astronauts or cosmonauts
.
© Mark Wade, 1997 - 2007 except where otherwise noted.
Encyclopedia Astronautica
topic index
0 -
A -
B -
C -
D -
E -
F -
G -
H -
I -
J -
K -
L -
M -
N -
O -
P -
Q -
Ra -
Re -
Sa -
Sf -
Sp -
T -
U -
V -
W -
X -
Y -
Z
Enter your search terms
Web
www.astronautix.com
Submit search form