AGM-88 HARM

[Chizh]

Wanted AGM-88 motor data.

Also any official specifications.

[Vitormouraa]

It's happening!

 

This might be useful:

 

http://www.bga-aeroweb.com/Defense/AGM-88-HARM-AARGM.html

http://www.designation-systems.net/dusrm/m-88.html

http://www.ausairpower.net/API-AGM-88-HARM.html

http://www.navy.mil/navydata/fact_display.asp?cid=2200&tid=300&ct=2

http://www.globalsecurity.org/military/library/policy/navy/ntsp/agm-88-d_2002.pdf

http://www.dtic.mil/ndia/2009gunmissile/AARGM.pdf

Edited October 26, 2016 by Vitormouraa

[BIGNEWY]

Wanted AGM-88 motor data.

Also any official specifications.

 

please stay on topic guys.

 

thanks

[Foka1]

3 minutes of google gives me this:

 

Thiokol SR113-TC-1 dual-thrust solid-fueled rocket

 

Thiokol AGM-88 HARM Motor

 

Length: 83.5 inches

Diameter: 10~ inches

Casing: D6AC steel

Propellant: 280 lbs of non-aluminized HTPB propellant

 

Notes: Reduced smoke, dual thrust boost/sustain motor.

 

References:

Jane’s All the World’s Aircraft 1981-82

 

 

 

But nowadays Raytheon make those missiles and they upgrading it.

[NineLine]

Assume ED knows how to use google ;) They are looking for deeper cut stuff I am sure...

[Tricky11]

This may help (see attached file)

93Sep_Chang.pdf

[iLOVEwindmills]

http://ausairpower.net/API-AGM-88-HARM.html

 

Ausair has a fairly extensive article on the HARM, probably some useful info in there.

[NRG-Vampire]

one more: maybe it helps too - for F-4 Phantom and F-16 Falcon/Viper modules as well :bounce:

 

Unclassified Acquisition Report (Costs)

http://www.globalsecurity.org/military/library/budget/fy2013/sar/02_agm-88e_aargm__december2013_sar.pdf

 

 

 

ahhh :) some Wild Weasel mission would be exciting :thumbup: with a Hornet likewise

ps. btw, wondering what kind of rocket motor data is public and unclassified :dunno:

 

Edited October 26, 2016 by NRG-Vampire

[Rlaxoxo]

Assume ED knows how to use google ;) They are looking for deeper cut stuff I am sure...

 

While I was looking trough Missile_data.lua code I saw a SAM slight missile data and there was a link next to "Engine burn time"

 

It was a youtube video of Missile spining out of control before exploding after 10 seconds

[Curly]

National Stock Numbers confirm the the motor is model Ysr-113-tc-1 it weighs 387 lbs and contains 280 lbs of propellant. The propellant is listed as Tp-11-1159.

https://nationalstocknumber.info/national-stock-number/1337-01-162-3421

 

This claim is backed by secondary sources in the NASA and DTIC databases.

 

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19870011601.pdf

Page 3-194 in the NASA doc

 

http://www.dtic.mil/dtic/tr/fulltext/u2/a342309.pdf

Page 9: the fuel type and composition is listed.

 

Specifications for this fuel can be found in Johns Hopkins Chemical Propulsion Information Agency “Solid Propellant Manual”. The manual may also be know as “Solid Propellant Mechanical Behavior Manual”. The agency since has be renamed and can be found here. https://www.erg.jhu.edu/

The work does not appear to be publicly available.

[C3PO]

This may help (see attached file)

 

Super read! Really interesting.