Payload Performance
Note: Payload
performance and estimated cost provided for information only. If you are interested
in contracting for launch services, we recommend that you contact the service provider
directly using the information above.
| |
366 x
695 km
143° retrograde |
Estimated Launch Price |
Configuration |
Shavit 1
(AUS-51) |
500 lbm
225 kg |
US
$10-15 M |
Three
Stage Solid Propellant |
* Performance provided by
AIAA, "International Reference Guide to Space Launch
Systems", 3rd edition.
Vehicle Configuration
| |
Stage 1 |
Stage 2 |
Stage
3 |
| Length |
21.3 ft
6.5 m |
17.4 ft
5.3 m |
8.5 ft
2.6 m |
| Diameter |
4.4 ft
1.35 m |
4.4 ft
1.35 m |
4.4 ft
1.35 m |
| Gross Mass |
Roughly
13 t
(29 klbm) |
9.1
t
(20klbm) |
Roughly
2 t (4400 klbm) |
Propellant
Propellant Mass |
HTPB
28,100 lbm
12,750 kg |
HTPB
? lbm
? kg |
HTPB
4200 lbm
1900 kg |
Engine
Thrust (vacuum)
Isp (vacuum) |
? |
? |
AUS-51
|
| Number of Engines |
1 |
1 |
1 |
| Nominal Burn Time |
?
|
? |
92 s ? |
|
