Difference between revisions of "Demo parts"
From Kerbal Space Program Wiki
Casualology (talk | contribs) (→Landing Gear) |
|||
| (9 intermediate revisions by 7 users not shown) | |||
| Line 1: | Line 1: | ||
| − | [[File:All-parts-rocket-0.18.3.png|thumb|A four-stage rocket featuring every part available in the demo.]] | + | [[File:All-parts-rocket-0.18.3.png|thumb|A four-stage rocket featuring every part available in the old .18.3 demo.]] |
| + | [[File:MinmusDemo.jpeg|thumb|A very happy Kerbal on the surface of Minmus in the most recent 1.0 demo.]] | ||
| − | + | In the [[demo]] of [[Kerbal Space Program]], there is a more limited selection of parts than in the full game. | |
| − | |||
| − | |||
== Pods == | == Pods == | ||
| Line 50: | Line 49: | ||
==== Landing Gear ==== | ==== Landing Gear ==== | ||
{{Stats Table Landing Gear (Demo)}} | {{Stats Table Landing Gear (Demo)}} | ||
| + | The LT-1 Landing Strut is the only landing gear available in the demo. | ||
== Science == | == Science == | ||
| − | + | The Mystery Goo and Science Jr. are available in the 1.0 demo. | |
{{Demo parts}} | {{Demo parts}} | ||
Latest revision as of 23:16, 31 March 2023
In the demo of Kerbal Space Program, there is a more limited selection of parts than in the full game.
Pods
| Image | Part | Radial size | Cost (  ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
rotPower (kN·m) |
Crew |
|---|---|---|---|---|---|---|---|---|---|
|
Command Pod Mk1 | Small, Tiny | 600 | 0.8 | 0.2 | 3 400 | 14 | 5 | 1 
|
|
Stayputnik Mk. 1 | Tiny | 300 | 0.05 | 0.15-0.2 | 1800 | 12 | 0 | N/A |
Propulsion
Liquid Fuel Engines
| Fuel (≈t/s) | Isp (s) | TVC | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Radial size | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
Thrust (kN) |
T/W ratio | atm | vac | atm | vac | Gimbal (°) |
 |
LV-T30 Liquid Fuel Engine | Small | 850 | 1.25 | 0.2 | 3 600 | 7 | 215 | 17.5 | 0.0685 | 0.0592 | 320 | 370 | – |
Solid Fuel Boosters
| Solid Fuel Density is 7,5 kg/unit | Mass (t) | T/W ratio | Burn (s) | Isp (s) | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Size | Cost ( )
|
Full | Empty | Fuel (  )
|
Drag | Max Temp (K) |
Tolerance | Thrust (vac)(kN) |
Full | Empty | atm | vac | atm | vac |
 |
RT-10 Solid Fuel Booster | Small | 450 | 3 | 0.5 | 433 | 0.3 | 2 000 | 7 | 227 | 6.8 | 51.0 | 29 | 31 | 225 | 240 |
|
RT-5 "Flea" Solid Fuel Booster | Small | 320 | 1.2 | 0.45 | 100 | 0.2-0.3 | 2000 | 7 | 180 | ? | ? | 6 | 7 | 168 | 180 |
Liquid Fuel Tanks
| Rocket fuel density is 5 kg/unit | Mass (t) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Radial size | Cost ( ) |
Full | Empty | Drag | Max. Temp. (K) |
Fuel ( )
|
Oxidizer ( )
|
Impact tolerance (m/s) |
|
FL-T100 Fuel Tank | Small | 250 | 0.5625 | 0.06 | 0.2 | 2000 | 45 | 55 | 6 |
|
FL-T200 Fuel Tank | Small | 425 | 1.125 | 0.13 | 0.2-0.3 | 2000 | 90 | 110 | 6 |
RCS Fuel Tanks
| RCS Fuel Density is 4 kg/unit | Mass (t) | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Radial size | Cost ( ) |
Full | Empty | Drag | Max. Temp. (K) |
Tolerance (m/s) |
Fuel ( )
|
|
Stratus-V Roundified Monopropellant Tank | Radial mounted | 400 (352) |
0.315 | 0.05 | 2 | 2000 | 12 | 60 |
Control
SAS
| Image | Part | Radial size | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
Torque (kN·m) |
|---|---|---|---|---|---|---|---|---|
|
Small Inline Reaction Wheel | Small | 600 | 0.05 | 0.2 | 2 000 | 9 | 5 |
RCS
| Isp (s) | |||||||||
|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
Thrust (kN) | atm | vac |
 |
RV-105 RCS Thruster Block | 620 | 0.05 | 0.001 | 2000 | 15 | 1 | 100 | 240 |
Structural
Decouplers and Separators
| Image | Part | Radial size | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
Ejection force |
|---|---|---|---|---|---|---|---|---|
 |
TT-38K Radial Decoupler | Radial mounted | 600 | 0.025 | 0.2 | 2000 | 8 | 250 |
 |
TR-18A Stack Decoupler | Small | 400 | 0.05 | 0.2 | 2000 | 9 | 250 |
Adapters, Couplers & Struts
| Image | Part | Radial size | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
|---|---|---|---|---|---|---|---|
 |
TVR-1180C Mk1 Stack Tri-Coupler | Small, Small x 3 | 680 | 0.15 | 0.3 | 3 400 | 12 |
 |
EAS-4 Strut Connector | Radial mounted | 250 | 0.05 | 0.02 | 3 600 | 12 |
 |
FTX-2 External Fuel Duct | Radial mounted | 250 | 0.05 | 0.02 | 3 600 | 12 |
Ground Support
| Image | Part | Cost ( )
|
Max Temp (K) | Tolerance |
|---|---|---|---|---|
|
200 | 5000 | 100 |
Aerodynamic
Nose Cones
| Image | Part | Radial size | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
|---|---|---|---|---|---|---|---|
 |
Aerodynamic Nose Cone | Small | 680 | 0.03 | 0.3 | 3 400 | 10 |
Wings and Wing Parts
| Image | Part | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
Lift |
|---|---|---|---|---|---|---|---|
 |
AV-T1 Winglet | 500 | 0.05 | 0.5 | 3 400 | 12 | 0.3 |
Controlled Wings and Surfaces
| Image | Part | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
Lift | Deflection Range (°) |
Surface Area |
|---|---|---|---|---|---|---|---|---|---|
 |
AV-R8 Winglet | 500 | 0.02 | 0.02 | 3 400 | 12 | 0.4 | 15 | 0.95 |
Utility
Parachutes
| Drag | Deployment | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| Image | Part | Radial size | Cost ( ) |
Mass (t) |
Stowed | Semi-Deployed | Fully Deployed | Semi-Deploy Pressure (atm) |
Full-Deploy Altitude (m AGL) |
 |
Mk16 Parachute | Tiny | 422 | 0.1 | 0.22 | 1 | 500 | 0.01 | 500 |
Ladders
| Image | Part | Cost ( ) |
Mass (t) |
Drag | Max. Temp. (K) |
Tolerance (m/s) |
|---|---|---|---|---|---|---|
 |
Pegasus I Mobility Enhancer | 100 | 0.005 | 0.2 | 3 200 | 8 |
 |
Telus Mobility Enhancer | 100 | 0.005 | 0.2 | 3 200 | 8 |
Landing Gear
Template:Stats Table Landing Gear (Demo) The LT-1 Landing Strut is the only landing gear available in the demo.
Science
The Mystery Goo and Science Jr. are available in the 1.0 demo.
| ||||||||||||||||||||||||||||
