Jump to content
Main menu
Main menu
move to sidebar
hide
Navigation
Main page
Recent changes
Random page
Help about MediaWiki
Special pages
Niidae Wiki
Search
Search
Appearance
Create account
Log in
Personal tools
Create account
Log in
Pages for logged out editors
learn more
Contributions
Talk
Editing
CIM-10 Bomarc
(section)
Page
Discussion
English
Read
Edit
View history
Tools
Tools
move to sidebar
hide
Actions
Read
Edit
View history
General
What links here
Related changes
Page information
Appearance
move to sidebar
hide
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
===Bomarc B=== The liquid-fuel booster of the Bomarc A had several drawbacks. It took two minutes to fuel before launch, which could be a long time in high-speed intercepts, and its [[hypergolic propellant]]s (hydrazine and nitric acid) were very dangerous to handle, leading to several serious accidents.<ref name="Gibson"/> As soon as high-thrust [[solid-fuel rocket]]s became a reality in the mid-1950s, the USAF began to develop a new solid-fueled Bomarc variant, the IM-99B Bomarc B. It used a [[Thiokol]] XM51 booster, and also had improved Marquardt RJ43-MA-7 (and finally the RJ43-MA-11) ramjets. The first IM-99B was launched in May 1959, but problems with the new propulsion system delayed the first fully successful flight until July 1960, when a supersonic [[SSM-N-9 Regulus II|MQM-15A Regulus II]] drone was intercepted. Because the new booster required less space in the missile, more ramjet fuel could be carried, thus increasing the range to {{convert|700|km|mi|abbr=on|order=flip}}. The terminal homing system was also improved, using the world's first [[Pulse-Doppler radar|pulse Doppler search radar]], the Westinghouse AN/DPN-53.<ref name="ReferenceA"/> All Bomarc Bs were equipped with the W-40 nuclear warhead. In June 1961, the first IM-99B squadron became operational, and Bomarc B quickly replaced most Bomarc A missiles.<ref name="Gibson"/> On 23 March 1961, a Bomarc B successfully intercepted a Regulus II cruise missile flying at {{cvt|100000|ft|m}}, thus achieving the highest interception in the world up to that date. Boeing built 570 Bomarc missiles between 1957 and 1964, 269 CIM-10A, 301 CIM-10B.<ref name="Gibson"/> [[File:4751st Air Defense Squadron - ADC - Emblem.png|thumb|125px|4751st ADMS (Training) Emblem]] In September 1958 Air Research & Development Command decided to transfer the Bomarc program from its testing at Cape Canaveral Air Force Station to a new facility on [[Santa Rosa Island (Florida)|Santa Rosa Island]], south of Eglin AFB [[Hurlburt Field]] on the [[Gulf of Mexico]]. To operate the facility and to provide training and operational evaluation in the missile program, [[Aerospace Defense Command|Air Defense Command]] established the 4751st Air Defense Wing (Missile) (4751st ADW) on 15 January 1958. The first launch from Santa Rosa took place on 15 January 1959.<ref name="Gibson"/>
Summary:
Please note that all contributions to Niidae Wiki may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see
Encyclopedia:Copyrights
for details).
Do not submit copyrighted work without permission!
Cancel
Editing help
(opens in new window)
Search
Search
Editing
CIM-10 Bomarc
(section)
Add topic