Difference between revisions of "GSM.38 Jupiter ASM"

Revision as of 13:32, 7 June 2007

Jupiter

Profile (n/a)

Design details (GSM.38)
Function	ASM, SSM, SLCM
Manufacturer	Harker-Boss Precision Rocketry
Design No.	PASM-91
Unit cost	$134 Million
Service dates	2006-present
General characteristics
Length	25.2m
Diameter	2.6m
Finspan	Not Released
Wingspan	Not Released
Launch mass	96 Tons
Flight characteristics
Propulsion	NP-M-65 Rocket Booster NP-139H RAMjet Booster to PDE NP-M-127 SCRAMjet/PDE
Flight control	[Adaptive Skin] Forward Thrust Nozzels [[http://www.nasa.gov/centers/dryden/news/FactSheets/FS-061-DFRC.html%7CActive-Aeroelastic Wings}}
Speed
Manoeuvrability	>12g
Range
Ceiling
Guidance and payload
Guidance	Midcourse: GPS/INS, AOSAM, command uplink Terminal: Dual-mode radar with IIR and automatic target recognition
Warhead	500 kg BROACH APHE
Fuzes	Timed penetrator, contact
Launch platforms
Ship
Land
Operators
Artitsan Imperial Navy \| Artitsan Imperial Airforce

Surface-to-surface missiles
Ahab \| Battle Axe \| Doomsday \| Hájord \| Hatchet \| Hurricane \| Jupiter \| HyStrike \| Khan \| Pelican \| Sicarius \| Starbolt \| Stryker \| Vidofnir \| Yakhont 3

@@ Line 46: / Line 46: @@
 |-
 |style="vertical-align:top; text-align:right; font-weight:bold;"|Propulsion
-|Nolan-Petyav NP-M-65 Rocket Booster
+|NP-M-65 Rocket Booster<br>NP-139H RAMjet Booster to PDE<br>NP-M-127 SCRAMjet/PDE
-|Nolan-Petyav NP-139H RAMjet Booster to PDE
-|Nolan-Petyav NP-M-120 SCRAMjet/PDE
 |- style="background:#f0f0f0;"
 |style="vertical-align:top; text-align:right; font-weight:bold;"|Flight control
-|
+|[[http://www.highbeam.com/doc/1G1-8954223.html|Mission Adaptive Skin]]<br>Forward Thrust Nozzels<br>[[http://www.nasa.gov/centers/dryden/news/FactSheets/FS-061-DFRC.html|Active-Aeroelastic Wings}}<br>
 |-
 |style="vertical-align:top; text-align:right; font-weight:bold;"|Speed