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I actually wanted to avoid double postsYou wanted this post here too?
I actually wanted to avoid double postsYou wanted this post here too?
A quoted reply doesn't count as a double post.I actually wanted to avoid double posts![]()
JASSM was allways 25.3 in wide. Neither B or C changed that. For some reason i can't find the factsheet on AF.mil anymore but they also stated this under there pictures:Cross post: https://www.secretprojects.co.uk/th...the-northrop-grumman-f-a-xx.50922/post-871282
Help appreciated!
Many thanks - It fitsThe information on wikipedia is a direct citation of official millitary publication.
For some reason these discrepancies happen a lot even with authentic informations. *shrugs*
also caled "180 Inch Rotary Launcher"
L: 178.00"
So where did the 22" number come from?JASSM was allways 25.3 in wide. Neither B or C changed that. For some reason i can't find the factsheet on AF.mil anymore but they also stated this under there pictures:
AGM-158 Joint Air-to-Surface Stand-off Missile (JASSM). GPS/INS-guided air-to-surface powered missile. Dimensions: Length 14 ft., width 25.3 in. Range: more than 230 miles. Image created by Billy Smallwood of the Air Force News Agency and is 8x2 inches @ 300ppi.
https://www.af.mil/About-Us/The-Book/Enlisted-Ranks/igphoto/2000420243/
WikipediaSo where did the 22" number come from?
And where TF did Wikipedia get it? Janes? Who here has a Jane's subscription?Wikipedia
I don't know but USAF stated everytime that JASSM and JASSM-ER have the same dimensions (in that regard). Likely some confusion or older numberSo where did the 22" number come from?
Yes wasn't that this laminate flow wing ? I remember the discussion we had here quite some time ago. While i can see how this could lead to a larger width but i stay by my statement that it allways was around 25 inches.For reasons at hand I'm not going to discuss this any further
but there are two key informations you don't know or figured or found out yet.
The wings are different.
Around 0,3m more tho if this impacted the diameter?The wing spans are different.
Between LRASM and JASSM?For reasons at hand I'm not going to discuss this any further
but there are two key informations you don't know or figured or found out yet.
The wings are different.
The wing spans are different.
I assume more lift while reducing drag, hence, chord length got longer which increases folded width.Yes wasn't that this laminate flow wing ? I remember the discussion we had here quite some time ago. While i can see how this could lead to a larger width but i stay by my statement that it allways was around 25 inches.
*https://www.secretprojects.co.uk/threads/agm-158-jassm.1974/post-311298
Around 0,3m more tho if this impacted the diameter?
Between A-JASSM and B-JASSM-ER.Between LRASM and JASSM?
Shows longer wingspan, not wider stowed wings.I assume more lift while reducing drag, hence, chord length got longer which increases folded width.
Between A-JASSM and B-JASSM-ER.
It looks like one site still has the old data recorded and not fixed-aligned like with most everyone's copy paste or falsely-assumption-autofixed-it etc.
Okay, that makes sense.I assume more lift while reducing drag, hence, chord length got longer which increases folded width.
Between A-JASSM and B-JASSM-ER.
And where is that on the site you linked? Because all I'm seeing is this:here's a screenshot from a site by a group of navy ex-militaries "highlighted the relevant part":
View attachment 799051
Specifications
Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!
Data for AGM-158A/B:
AGM-158A AGM-158B Length 4.29 m (14 ft 1 in) Wingspan 2.4 m (7 ft 11 in) 2.7 m (8 ft 10 in) Weight 1020 kg (2250 lb) 1200 kg (2600 lb) Speed subsonic Range > 370 km (230 miles) > 925 km (575 miles) Propulsion Teledyne CAE J402-CA-100 turbojet; 3.0 kN (680 lb) Williams F107-WR-105 turbofan; 6.2 kN (1400 lb) Warhead 450 kg (1000 lb) WDU-42/B penetrator [merged cell in original]
Except this shows same wing length for all 3 missiles which yourself stated to be different.here's a screenshot from a site by a group of navy ex-militaries "highlighted the relevant part":
View attachment 799051
There is a more powerful explosive known as AFX-777 but I don't know of any missiles using it.I’m wondering whether different production batches of JASSM might use slightly different formulations or modified versions of AFX-757.
For example, could there be changes in the composition, material quality, or other adjustments between batches?
I would also be very interested in learning about any explosive iterations in other missiles that use AFX-757.
Do you have anything on it?There is a more powerful explosive known as AFX-777 but I don't know of any missiles using it.
Do you have anything on it?
JASSM uses a 5 - element CPRA :Evidence of JASSM being employed in Iran .....
https://osmp.ngo/model/agm-158-jassm-series/
“The Ministry of Defense is procuring additional Deep Precision Strike munitions to replenish operational stocks,” the report said, released on Wednesday. “Discussions with the U.S. government regarding the procurement of these munitions have now begun.”
uhm.A notice of intent released on Friday indicates that the U.S. Air Force plans to procure over 11,000 JASSM and LRASM missiles over the next five to seven years, significantly raising its inventory targets—targets that have been steadily increased over the past decade.
Procurement of JASSM will remain at high levels in fiscal years 2024–2025, with slight adjustments in 2026 due to budget and inventory considerations. A breakdown of projected JASSM and LRASM procurement for fiscal years 2024–2026 is provided below (based on publicly available budget and contract data).
11,000 in 5 years means an average of 2200/year.Thanks, I had not realized LRASM was being purchased at that level. Still low, IMO, but there should be many hundreds in inventory by now.
Last I heard, production per year had increased to 750 with a goal of 1100, and those numbers must be out of date given USAF goals.