McDonnell Douglas F/A-18 Hornet
aeronewsline :: Accueil :: Histoire :: Aéronefs 1976 à 1982
Page 12 sur 40
Page 12 sur 40 • 1 ... 7 ... 11, 12, 13 ... 26 ... 40
Re: McDonnell Douglas F/A-18 Hornet
Je reviens au chapitre principal McDonnell Douglas F/A-18 Hornet de Wikipedia.en
[Vous devez être inscrit et connecté pour voir ce lien]
---------------------------------------------------------------------------------------------------------------------
Other US variants
F-18(R)
This was a proposed reconnaissance version of the F/A-18A.
It included a sensor package that replaced the 20 mm cannon.
The first of two prototypes flew in August 1984.
Small numbers were produced.
[Vous devez être inscrit et connecté pour voir ce lien]
[Vous devez être inscrit et connecté pour voir ce lien]
---------------------------------------------------------------------------------------------------------------------
Other US variants
F-18(R)
This was a proposed reconnaissance version of the F/A-18A.
It included a sensor package that replaced the 20 mm cannon.
The first of two prototypes flew in August 1984.
Small numbers were produced.
[Vous devez être inscrit et connecté pour voir ce lien]
Trish- CLUB
- Messages : 5838
Re: McDonnell Douglas F/A-18 Hornet
RF-18D
Proposed two-seat reconnaissance version for the US Marine Corps in the mid-1980s.
It was to carry a radar reconnaissance pod.
The system was canceled after it was unfunded in 1988.
This ability was later realized on the F/A-18D(RC)
Proposed two-seat reconnaissance version for the US Marine Corps in the mid-1980s.
It was to carry a radar reconnaissance pod.
The system was canceled after it was unfunded in 1988.
This ability was later realized on the F/A-18D(RC)
Trish- CLUB
- Messages : 5838
Re: McDonnell Douglas F/A-18 Hornet
TF-18A
Two-seat training version of the F/A-18A fighter, later redesignated F/A-18B.
Two-seat training version of the F/A-18A fighter, later redesignated F/A-18B.
Trish- CLUB
- Messages : 5838
Re: McDonnell Douglas F/A-18 Hornet
F-18 HARV
Single-seat High Alpha Research Vehicle for NASA.
High angles of attack using thrust vectoring, modifications to the flight controls, and forebody strakes
Single-seat High Alpha Research Vehicle for NASA.
High angles of attack using thrust vectoring, modifications to the flight controls, and forebody strakes
Trish- CLUB
- Messages : 5838
Re: McDonnell Douglas F/A-18 Hornet
High Alpha Research Vehicle
[Vous devez être inscrit et connecté pour voir ce lien]
------------------------------------------------------------------"
The High Alpha (angle of attack) Research Vehicle was a modified F/A-18 Hornet used by NASA in a 3-phase program investigating controlled flight at high angles of attack using thrust vectoring, modifications to the flight controls, and with actuated forebody strakes.
The program lasted from April 1987 to September 1996.
NASA reported that in one phase of the project, Dryden Flight Research Center "research pilots Bill Dana and Ed Schneider completed the envelope expansion flights in February 1992.
Demonstrated capabilities included stable flight at approximately 70 degrees angle of attack (previous maximum was 55 degrees) and rolling at high rates at 65 degrees angle of attack.
Controlled rolling would have been nearly impossible above 35 degrees without vectoring."
Performance figures were not listed for other phases.
[Vous devez être inscrit et connecté pour voir ce lien]
------------------------------------------------------------------"
The High Alpha (angle of attack) Research Vehicle was a modified F/A-18 Hornet used by NASA in a 3-phase program investigating controlled flight at high angles of attack using thrust vectoring, modifications to the flight controls, and with actuated forebody strakes.
The program lasted from April 1987 to September 1996.
NASA reported that in one phase of the project, Dryden Flight Research Center "research pilots Bill Dana and Ed Schneider completed the envelope expansion flights in February 1992.
Demonstrated capabilities included stable flight at approximately 70 degrees angle of attack (previous maximum was 55 degrees) and rolling at high rates at 65 degrees angle of attack.
Controlled rolling would have been nearly impossible above 35 degrees without vectoring."
Performance figures were not listed for other phases.
Trish- CLUB
- Messages : 5838
Page 12 sur 40 • 1 ... 7 ... 11, 12, 13 ... 26 ... 40
Sujets similaires
» McDonnell Douglas F/A-18 Hornet
» McDonnell Douglas F/A-18 Hornet
» McDonnell Douglas MD-80
» McDonnell Douglas MD-80
» McDonnell Douglas MD-80
» McDonnell Douglas F/A-18 Hornet
» McDonnell Douglas MD-80
» McDonnell Douglas MD-80
» McDonnell Douglas MD-80
aeronewsline :: Accueil :: Histoire :: Aéronefs 1976 à 1982
Page 12 sur 40
Permission de ce forum:
Vous ne pouvez pas répondre aux sujets dans ce forum