Archive for November, 2007
TU95 vs F4, Middway
November 30, 2007
Lim
November 28, 2007
MiG 15 diagram
November 27, 2007
Massachusetts Faces a Test on Health Care
November 25, 2007http://www.nytimes.com/2007/11/25/us/politics/25mass.html?ref=us
A year after Massachusetts became the only state to require that individuals have health coverage, residents face deadlines to sign up or lose their personal tax exemption, worth $219 on next year’s state income tax returns. More than 200,000 previously uninsured residents have enrolled, but state officials estimate that at least that number, and perhaps twice as many, have not.
Those managing the enrollment effort say it has exceeded expectations. In particular, state-subsidized insurance packages offered to low-income residents have been so popular that the program’s spending may exceed its budget by nearly $150 million.
Senator Barack Obama of Illinois sees it a different way. He argues there is danger in mandating coverage before it is clear it can be affordable for those at the margins. While Mr. Obama does not rule out a mandate down the road, his emphasis is on reducing costs and providing generous government subsidies to those who need them. He would mandate coverage for children.
МиГ-21 diagram
November 25, 2007
РУКОТВОРНЫЕ МОЛНИИ RUKOTVORNYE MOLNII
http://mkmagazin.almanacwhf.ru/avia/mig_21f_13.htm
СВЕРХЗВУКОВЫЕ РЕАКТИВНЫЕ ИСТРЕБИТЕЛИ SVERHZVUKOVYE REAKTIVNYE ISTREBITELI
|
МиГ-21Ф-13 MiG-21F-13 |
“ Мираж-111С ” “Mirazh-111S” |
F-104G |
SAAB-35D |
F-5E |
|
|
Размах крыла, м Wingspan, m |
7,154 7154 |
8,2 8.2 |
6,68 6.68 |
9,4 9.4 |
8,14 8.14 |
|
Длина самолета, м The length of the aircraft, m |
15,76 15.76 |
13,83 13.83 |
16,69 16.69 |
15,35 15.35 |
14,69 14.69 |
|
Площадь крыла, м2 Area wing m2 |
23,0 23.0 |
34,1 34.1 |
18,28 18.28 |
49,2 49.2 |
17,29 17.29 |
|
Тяга двигателя, кгс Engine Thrust, kgs |
5750 |
6200 |
7167 |
8000 |
2Х2268 2 H2268 |
|
Взлетный вес, кгс Take-off weight kgs |
7570 |
11800 |
9510 |
11400 |
6985 |
|
Скорость км/ч Speed km / h |
2125 |
2220 |
2120 |
2100 |
1700 |
|
на высоте, м at the height m |
12500 |
12000 |
12200 |
11500 |
11000 |
|
Скорость у земли, км/ч The speed of the land km / h |
1490 |
1470 |
1400 |
1200 |
|
|
Потолок, м Ceiling, m |
19000 |
23000 |
17680 |
16700 |
16300 |
|
Дальность полета, км Range km |
1580 |
650 |
819 |
635 |
1400 |
|
Вооружение: пушечное, шт/калибр Armament: gun, pc / Caliber |
1Х30 1 H30 |
2Х30 2 H30 |
1Х20 1 H20 |
2Х30 2 H30 |
2Х20 2 H20 |
|
ракетное, кол-во ракет “ воздух — воздух ” the missile, number of missiles and air-to-air “ |
2 |
2 |
4 |
4 |
2 |
СВЕРХЗВУКОВОЙ ИСТРЕБИТЕЛЬ МИГ-21Ф-13 SVERHZVUKOVOY ISTREBITEL MIG-21F-13
Реактивный сверхзвуковой самолет-истребитель МиГ-21 Ф-13: 1 — подвижный конус (центральное тело регулируемого воздухозаборника), 2 — штанга приемника воздушного давления, 3 — отсеки оборудования, 4 — катапультируемое кресло пилота, 5 — топливные баки, 6 — замок тормозного парашюта, 7 — контейнер тормозного парашюта, 8 — двигатель Р-11Ф-300, 9 — тормозные щитки, 10 — антенна радиолокационного прицела, 11 — канал воздухозаборника двигателя, 12 — аэродинамические гребни на крыле , 13 — противофлаттерные балансиры стабилизатора, 14 — ракеты “ воздух— воздух ” К-13, 15 — пушка, 16 — подвесной топливный бак, 17 — створки дополнительного забора воздуха, 18 — воздухозаборники для обдува двигателя, 19—закрылок, 20—цельноповоротное горизонтальное оперение. Supersonic Jet aircraft MiG-21 F-13: 1-rolling cone (central body adjustable air), 2-pole receiver air pressure, 3-separation equipment, 4-Ejection pilot’s seat, 5-Tanks, 6-lock brake parachute, 7-container braking parachute, 8-engine R-11F-300, 9-brake pads, 10-antenna radar sight, 11-channel air engine, 12-aerodynamic ridges on the wing, 13-protivoflatternye balances stabilizer, a 14-missiles “air-air” K-13, 15-gun, 16-hanging fuel tank, 17-leaf additional air fence, 18-Air airflow to the engine, 19-zakrylok, 20-tselnopovorotnoe horizontal of feathers.
