Talk:PL-15: Difference between revisions
Appearance
Content deleted Content added
MilHistBot (talk | contribs) Automatic MILHIST checklist assessment - Start class |
→clarification of text needed: new section |
||
Line 5: | Line 5: | ||
Hi, I removed the citation for this missile being available for the JF-17 because "Military Watch Magazine" is an amateur blog with a lot of wild unsubstantiated claims. [[User:Ghost1736|Ghost1736]] ([[User talk:Ghost1736|talk]]) 05:40, 7 December 2019 (UTC) |
Hi, I removed the citation for this missile being available for the JF-17 because "Military Watch Magazine" is an amateur blog with a lot of wild unsubstantiated claims. [[User:Ghost1736|Ghost1736]] ([[User talk:Ghost1736|talk]]) 05:40, 7 December 2019 (UTC) |
||
== clarification of text needed == |
|||
What is this supposed to mean: |
|||
"Compared to ramjet-powered Meteor, which advantages in sustained flight profile with a fly-out speed between Mach 3 and 3.5, the dual-pulsed solid propellant rocket motor of PL-15 potentially offers higher burn-out speed excess of Mach 5, then gradually loses its velocity at the terminal phase." |
|||
If it intends to say, "the Meteor has advantages in sustained flight..." please omit the comma after Meteor. |
|||
Also, the phrase "which advantages" is awkward perhaps "with advantages" would be better. [[Special:Contributions/75.72.161.233|75.72.161.233]] ([[User talk:75.72.161.233|talk]]) 18:55, 6 August 2023 (UTC) |
Revision as of 18:55, 6 August 2023
China Start‑class Low‑importance | ||||||||||
|
Military history: Technology / Weaponry / Asian / Chinese Start‑class | |||||||||||||||||||||||||||||||||||||
|
Military Watch Magazine - source credibility
Hi, I removed the citation for this missile being available for the JF-17 because "Military Watch Magazine" is an amateur blog with a lot of wild unsubstantiated claims. Ghost1736 (talk) 05:40, 7 December 2019 (UTC)
clarification of text needed
What is this supposed to mean: "Compared to ramjet-powered Meteor, which advantages in sustained flight profile with a fly-out speed between Mach 3 and 3.5, the dual-pulsed solid propellant rocket motor of PL-15 potentially offers higher burn-out speed excess of Mach 5, then gradually loses its velocity at the terminal phase."
If it intends to say, "the Meteor has advantages in sustained flight..." please omit the comma after Meteor.
Also, the phrase "which advantages" is awkward perhaps "with advantages" would be better. 75.72.161.233 (talk) 18:55, 6 August 2023 (UTC)
Categories:
- Start-Class China-related articles
- Low-importance China-related articles
- Start-Class China-related articles of Low-importance
- WikiProject China articles
- Start-Class military history articles
- Start-Class military science, technology, and theory articles
- Military science, technology, and theory task force articles
- Start-Class weaponry articles
- Weaponry task force articles
- Start-Class Asian military history articles
- Asian military history task force articles
- Start-Class Chinese military history articles
- Chinese military history task force articles