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Lockheed C-130 Hercules (12 pics)
NZ7003, A New Zealand Air Force C-130H
Delivered in April 1965 together with 7001 and 7002, The first production C-130H's
|
The C-130 Hercules is still longer in production than any
aircraft in history. The C-130 Hercules was first flown in the form of a YC-130
prototype on August 23, 1954, first delivery to the USAF in December 1956. The
C-130 design is based on a high wing, unobstructed cargo compartment, roll
on/off ramp, palletized cargo floor, and flat level floor at truck-bed height
above the ground.
The
current basic transport Hercules, the C-130H was first delivered in April 1975,
can be configured for cargo (5 463L pallets), paratroopers (64), combat troops
(92), hospital litter patients (74), or any combinations of all of these.
The aircraft is capable of
operating from rough, dirt strips and is the prime transport for Para dropping
troops and equipment into hostile areas. Basic and specialized versions perform
a diversity of roles, including airlift support, DEW Line and Arctic ice
resupply, aero medical missions, aerial spray missions, fire-fighting duties for
the US Forest Service, and natural disaster relief missions. In recent years,
they have been used to bring humanitarian relief to many countries, including
Haiti, Bosnia, Somalia, and Rwanda.
The
L-100-20/30 Hercules is the stretched civilian version of the C-130H basic
military model.
First flight of the new
high-tech variant, C-130J-30 (RAF Hercules C4 ZH865) was on April 5, 1996. The
C-130J's new engine is the AE2100B3 with a new six-blade propeller, the cockpit
has new flight control systems (glass-cockpit).
Lockheed C-130J Hercules
The C-130J incorporates
state-of-the-art technology that significantly improves performance and reduces
ownership costs. Lockheed Martin projections show the C-130J/J-30 will lower
cost of ownership as much as 45% depending on the scenario used. Early model
C-130s require more than 20 maintenance man-hours per flight hour (MMH/FH). The
C-130J/J-30 will require 10 or less MMH/FH. The C-130J/J-30 integrated digital
technology provides the capability to airdrop in instrument conditions without
zone markers, as a baseline feature of the aircraft. When the high resolution
ground mapping capability of the APN-241 Low Power Color Radar is coupled with
the dual INS/GPS and digital mapping systems, the C-130J/J-30 provides
single-ship or formation all weather aerial delivery. This means the entire
J/J-30 fleet will be all weather airdrop capable. C-130Js will be delivered as
weather (WC), electronic combat (EC), and tanker (KC) configured aircraft.
The United States Marine Corps has
chosen the KC-130J tanker to replace its aging KC-130F tanker fleet. The new
KC-130J offers increased utility and much needed improvement in mission
performance. As a force multiplier, the J tanker is capable of refueling both
fixed wing and rotary wing aircraft as well as conducting rapid ground
refueling. The refueling speed envelope has been widened from 100 to 270 knots
indicated airspeed, offering more capability and flexibility. Offload rates per
refueling pod can be up to 300 gallons / 2,040 lbs (1,135 liters / 925 kg) per
minute simultaneously. The J tanker's offload is significantly greater than
previous Herc tankers. As an example, at 1,000 nautical miles, the fuel offload
is well over 45,000 lbs. Rapid ground refueling is also a premium capability. In
austere conditions/scenarios, the KC-130J can refuel helicopters, vehicles, and
fuel caches at 600 gallons / 4,080 lbs (2,270 liters / 1,850 kg) per minute.
Additionally, the unique prop feathering capability while the engines are still
running ("HOTEL Mode") offers safer and more hospitable conditions for ground
refueling than in the past.
The WC-130J Hercules is a special
weather reconnaissance version of the new Lockheed Martin C-130J cargo plane.
Its mission is to fly into the eye of hurricanes to retrieve critical
information about active storms. The Air Force Reserve Command's 53rd Weather
Reconnaissance Squadron at Keesler Air Force Base, MS, a component of the 403rd
Wing, is the only unit in the Department of Defense that flies this mission.
The standard C-130J has
essentially the same dimensions as the C-130E/H but the J-30 (stretched version)
is 15 feet longer. The J-30 incorporates two extension plugs, one forward and
one aft. The forward plug is 100 inches long while the rear plug is 80 inches for
a total of 180 inches or 15 feet. With its 3,000 nautical mile range, increased
speed, and air refueling capability, it complements the C-5/C-17 airlift team.
The J-30 can work in the strategic, as well as tactical or intratheater,
environment. The J-30 can be an effective force multiplier in executing the US
Army Strategic Brigade Airdrop (SBA). The J-30 can airdrop 100% of the SBA
requirement. No longer is it necessary to expend scarce heavy lift resources on
strategic contingency requirements. Whether it's a channel, special airlift,
training, or contingency airdrop mission, the J-30 can handle it all at a
significantly reduced cost.
For the first time in the 40-plus
year history of the popular Hercules transport, the US Air Force and Lockheed
Martin Aeronautical Systems signed a commercial practices contract for the sale
of C-130Js. Awarded on 06 November 1996, the basic contract includes an initial
order for two aircraft, associated data, and spares, funded in fiscal year 1996.
The contract also contains five years of options through the year 2000 for
additional aircraft, interim contractor support, data, training, and support. By
late 1996 Aeronautical Systems had completed assembly of the first "production"
C-130J (Serial # 5440), one of 12 ordered by the Royal Australian Air Force.
Lockheed C-130 Special Missions Aircraft
MC-130E (Rivet Clamp) (Rivet Swap) (Rivet
Yank) Three distinct versions of this model: Nine aircraft are of the Rivet
Clamp version fitted with the Fulton recovery yoke together with an infra-red
detection system, chaff / flare dispensers, and a tail cone-mounted radar
warning receiver. Three Rivet Yank are similarly configured but lack the Fulton
system and have T56-A-15 engines fitted, while the two Rivet Swap Hercules
appear to be system evaluation aircraft.
EC-130E Rivet Rider witch are operated by the
Pennsylvania ANG for psychological warfare duties. The Rivet Riders feature a
large blade antenna on the leading edge of the fin along with another curved
antenna beneath the wings outboard of the engines. Underwing pods and a rear
fuselage pod contain trailing wire antennas.
Specifications: EC-130E
Weight: empty 33.063 kg.
Maximum payload
20412 kg.
Speed: 612 km/h.
Range: 7564 km.
Performance: maximum rate of climb at
sea level 558 m per minute.
The HC-130N was fielded for rescue and for
recovery of space capsules. They have Cook Aerial Trackers to locate satellite
capsules during re-entry from orbit.
The HC-130P combined the rescue and recovery configuration
and added a tanker mission, having under-wing refueling drogue pods previously
developed for the US Marines KC-130F and used primarily to refuel rescue and
special-operation helicopters. |
|
Developing Nation: |
United States of America. |
|
Manufacturer/designer: |
Lockheed
Martin Aeronautics Company. |
| Production line: |
. |
|
Task: |
Global
airlift. |
|
First Flight: |
- YC-130A
August 23, 1954.
- C-130A April 7, 1955.
- C-130H November 1964.
- L-100-30 December 3, 1979.
-
C-130J-30 April 5, 1996, ZH865. |
|
First Delivery: |
- C-130A
December 1956.
- C-130B April 1959.
- C-130E April 1962.
- C-130H April 1965
- C-130H2 1978.
- C-130H3 1992.
- C-130J 1996.
- L-100 1964.
- L-100-20 1968.
- L-100-30 1970.
- C-130H-30
1980.
- C-130J-30 November 1999. |
| Last Delivery: |
- C-130A
November 1959.
- C-130B March 1963.
- C-130E March 1974.
- C-130H in production
- C-130H2 1992.
- C-130H3 1997.
- C-130J in production.
- L-100 December 1968.
- L-100-20 March 1981.
- L-100-30 in production.
-C-130H-30
1997. |
|
Crew: |
Five (two
pilots, navigator, flight engineer and loadmaster) |
| |
Lockheed C-130H Hercules |
|
Wing span: |
40,41 m. |
|
Wing area: |
161,12 m². |
| Wing aspect ratio: |
10,09 |
|
Length: |
29,79 m. |
| Fuselage diameter: |
3,22 m. |
|
Height: |
11,66 m. |
| Tail plane span: |
16,05 m. |
|
Wheel track: |
4,35 m. |
|
Wheelbase: |
9, 77m. |
| Cabin length: |
12.31
m. |
| Cabin diameter: |
3.12
m. |
|
Cabin height: |
2.74
m. |
| Rear ramp
length: |
3.12 m. |
| Rear ramp
width: |
3.02 m. |
| Cargo volume: |
127 m³. |
|
Engine (s): |
Four Allison
T56-A-15 turboprops each rated 4.591 hp. |
| Propeller: |
diameter 4.11 m. |
|
Weight: |
-
empty: 31.434 Kg.
- fuel: 19.116 liter.
- external fuel: 2
under wing
tanks 1703 liter.
- max. payload: 19.090
Kg. |
|
Max. Take off weight: |
69.750 kg. |
|
Max. Speed: |
Km/h.
366 mph |
| Max. cruise at low altitude: |
595 km/h. |
| Service ceiling: |
7.077 m
with 19,090 kg payload. |
|
Max. Range: |
km. |
|
Performance: |
- take-off run 1.311 m at
max. take-off weight.
- max. rate of climb at sea
level 610 m/min. |
| Under wing hard
points: |
2 |
| |
Lockheed C-130H-30
Hercules |
|
Crew: |
Five (two
pilots, navigator, flight engineer and loadmaster) |
|
Length: |
34,37 m. |
| Fuselage diameter: |
3,22 m. |
|
Height: |
11,66 m. |
| Tail plane span: |
16,05 m. |
|
Wheel track: |
4,35 m. |
| Cabin length: |
16,91
m. |
| Cabin diameter: |
3.12
m. |
|
Cabin height: |
2.74
m. |
| Rear ramp
length: |
3.12 m. |
| Rear ramp
width: |
3.02 m. |
| Cargo volume: |
170,5 m³. |
|
Engine (s): |
Four Allison
T56-A-15LFE turboprops each rated 4.591 hp. |
| Propeller: |
diameter 4.11 m. |
|
Weight: |
-
empty: 36.397
Kg.
- fuel: 19.116 liter.
- external fuel: 2
under wing
tanks 1703 liter.
- max. payload: 17.654
Kg. |
|
Max. Take off weight: |
79.310 kg. |
|
Max. Speed: |
602 Km/h. |
| Cruise speed: |
556 km/h. |
| Range: |
7.876 km. |
| Service ceiling: |
10.060 m. |
| |
Lockheed C-130J Hercules |
|
Crew: |
2 pilots and loadmaster. |
|
Length: |
29,79 m. |
| Fuselage diameter: |
3,22 m. |
|
Height: |
11,66 m. |
| Tail plane span: |
16,05 m. |
|
Wheel track: |
4,35 m. |
|
Wheelbase: |
9, 77 m. |
| Cabin length: |
12.31
m. |
| Cabin diameter: |
3.12
m. |
|
Cabin height: |
2.74
m. |
| Rear ramp
length: |
3.12 m. |
| Rear ramp
width: |
3.02 m. |
| Cargo volume: |
127,4 m³. |
| Combat delivery
capability: |
-
5 pallets.
-
74 litters.
- 16 cds bundles.
- 92 combat troops .
- 64 paratroops. |
|
Engine (s): |
Four
Rolls-Royce AE 2100D3 turboprops each rated 4.700 hp. |
| Propeller: |
Dowty Aerospace, all composite six blade R391
propellers diameter 4,15 m. |
|
Weight: |
-
empty: 34.275 Kg.
- fuel: 25.522 liter.
- external fuel: 2
under wing
tanks 1703 liter.
- max. payload: 19.090
Kg. |
|
Max. take off weight: |
70.305 kg. |
| Max. landing weight: |
58.965 kg. |
|
Max. speed: |
724 Km/h. |
| Service ceiling: |
7.077 m
with 19.090 kg payload. |
|
Performance: |
- take-off run 594 m at max.
take-off weight.
- max. rate of climb at sea
level 610 m/min. |
| |
Lockheed C-130J-30
Hercules |
|
Crew: |
2 pilots and loadmaster. |
|
Length: |
34,37 m. |
| Fuselage diameter: |
3,22 m. |
|
Height: |
11,66 m. |
| Tail plane span: |
16,05 m. |
|
Wheel track: |
4,35 m. |
|
Wheelbase: |
9,77 m. |
| Cabin length: |
16,91
m. |
| Cabin diameter: |
3.12
m. |
|
Cabin height: |
2.74
m. |
| Rear ramp
length: |
3.12 m. |
| Rear ramp
width: |
3.02 m. |
| Cargo volume: |
170,5 m³. |
| Combat delivery
capability: |
-
8 pallets.
-
97 litters.
- 24 cds bundles.
- 128 combat troops .
- 92 paratroops. |
|
Engine (s): |
Four
Rolls-Royce AE 2100D3 turboprops each rated 4.700 hp. |
| Propeller: |
Dowty Aerospace, all composite six blade R391
propellers diameter 4,15 m. |
|
Weight: |
-
empty: 35.996 Kg.
- fuel: 25.522 liter.
- external fuel: 2
under wing
tanks 1703 liter.
- max. payload: 20,227
Kg. |
|
Max. take off weight: |
74.393 kg. |
| Max. landing weight: |
58.965 kg. |
|
Max. speed: |
724 Km/h. |
| Max. range: |
5.556 km. |
| Service ceiling: |
7.077 m
with 19,090 kg payload. |
| C-130A variants: |
C-130B variants: |
C-130E variants: |
C-130H variants: |
L-100 commercial: |
|
YC-130 2
C-130A 204
C-130D 12
RC-130A 15
____________
233 |
C-130B 156
C-130F 7
HC-130B 12
KC-130F 46
LC-130F 4
WC-130F 5
_____________
230 |
C-130E 486
C-130G 4
EC-130E 1
___________
491 |
AC-130U 13
C-130H 690
C-130H-30 56
C-130HMP 4
C-130K
66
C-130T 20
EC-130V 1
EC-130Q 18
HC-130H 67
HC-130H-7 11
HC-130H(N) 6
HC-130N 15
HC-130P 20
KC-130H 22
KC-130R 14
KC-130T 26
KC-130T-30 2
LC-130H 7
LC-130R 6
MC-130H 24
_______________
1087 |
118 |
|
The Lockheed C-130 variants are in service by over 60 air
forces.
Military operators of the C-130 are:
|
| C-130A |
C-130B |
C-130E |
C-130H |
C-130H-30 |
L-100 |
C-130J |
|
Australia
Bolivia
Chad
Honduras
Mexico
Peru
United States:
CIA
USAF
USN |
Argentina
Bangladesh
Bolivia
Botswana
Columbia
Chile
Ecuador
Ethiopia
Greece
Indonesia
Jordan
Pakistan
Philippines
Romania
Singapore
South
Africa
Tunis
Turkey
United States:
USAF
USCG
USMC
USN
CIA |
Australia
Austria
Argentina
Brazil
Canada
Iran
Iraq
Israel
Mexico
Pakistan
Saudi Arabia
Sri Lanka
Sweden
United States:
USAF
USCG
CIA |
Abu Dhabi
Algeria
Argentina
Australia
Belgium
Bolivia
Brazil
Cameroon
Canada
Chad
Chile
Columbia
Denmark
Dubai
Egypt
France
Gabon
Greece
Indonesia
Iran
Israel
Italy
Japan
Jordan
Libya
Malaysia
Morocco
Netherlands
New Zealand
Niger
Nigeria
Norway
Oman
Philippines
Portugal
Romania
Saudi Arabia
Singapore
South-Korea
Spain
Sri Lanka
Sudan
Sweden
Taiwan
Thailand
Tunis
Turkey
United Kingdom
United States:
USAF
USCG
USMC
USN
NASA
Venezuela
Yemen
Zaire |
Algeria
Cameroon
Chad
Dubai
Egypt
France
Indonesia
Malaysia
Netherlands
Nigeria
Portugal
Saudi Arabia
South Korea
Thailand
United Kingdom
United States:
USMC |
Canada
Gabon
Indonesia
Kuwait
Pakistan
Peru
Philippines
UA Emirates
United States:
CIA
|
United Kingdom
Italy
United States
|
|
Missions |
Specialized Variant |
| Tactical Airlift |
All |
| Aerial Tanker |
KC-130B, KC-130F, KC-13H, HC-130H(N), HC-130N, HC-130P, KC-130R,
KC-130T, KC-130J |
| Command & Control |
EC-130E (ABCCC), EC-130G, & EC-130Q |
| Maritime Patrol |
C-130H-NP/PC-130H |
| Special Operations |
MC-130E, MC-130H, MC-130W |
| Search & Rescue |
SC-130B/HC-130B, HC-130E, HA-130H, HC-130H(N), HC-130N, &
HC-130P |
| Humanitarian Relief |
All |
| Staff/VIP Transport |
VC-130B & VC-130H |
| Reconnaissance |
RC-130B |
| Airborne Hospital |
C-130E (AEH) |
| Arctic & Anarctic Support |
C-130BL/LC-130F, C-130D, LC-130H, & LC-130R |
| Drone Control |
GC-130A/DC-130A, DC-130E, & DC-130H |
| Electronic Warfare |
EC-130E (CL), EC-130E (RR), EC-130H |
| Space & Missile Operations |
JC-130A, JC-130B, & NC-130H |
| Test & Evaluation |
NC-13A, NC-130B, JC-130E, NC-130E, JC-130H, & RC-130S |
| Weather Reconnaissance |
WC-130B, WC-130E, WC-130H, WC-130J |
| Gunship |
AC-130A, AC-130E, AC-130H, & AC-130U |
Lockheed C-130 Hercules
written-off by accidents:
|
? |
AT624 |
C-130H |
Nigerian Air Force |
|
02-09-1958 |
56-0528 |
C-130A-II |
USAF |
|
19-09-1958 |
56-0526 |
C-130A |
USAF |
|
20-05-1959 |
57-0468 |
C-130A |
USAF |
|
27-05-1961 |
59-1534 |
C-130B |
USAF |
|
..-10-1961 |
58-0745 |
C-130B |
USAF |
|
08-05-1962 |
55-0020 |
C-130A |
USAF |
|
17-05-1962 |
56-0546 |
C-130A |
USAF |
|
26-11-1962 |
56-0488 |
C-130A |
USAF |
|
27-08-1963 |
56-0474 |
C-130A |
USAF |
|
03-09-1964 |
T-1307 |
C-130B |
Indonesian Air Force |
|
11-01-1965 |
58-0719 |
C-130B |
USAF |
|
11-01-1965 |
58-0730 |
C-130B |
USAF |
|
25-03-1965 |
63-7797 |
C-130E |
USAF |
|
24-04-1965 |
57-0475 |
C-130A |
USAF |
|
01-07-1965 |
55-0039 |
C-130A |
USAF |
|
01-07-1965 |
55-0042 |
C-130A |
USAF |
|
18-08-1965 |
12648 |
C-130B |
Pakistan Air Force |
|
24-08-1965 |
149802 |
KC-130F |
US Marines |
|
18-09-1965 |
55-0038 |
C-130A |
USAF |
|
21-09-1965 |
T-1306 |
C-130B |
Indonesian Air Force |
|
08-12-1965 |
56-0502 |
C-130A |
USAF |
|
12-12-1965 |
56-0515 |
C-130A |
USAF |
|
20-12-1965 |
62-1843 |
C-130A |
USAF |
|
06-01-1966 |
61-0972 |
C-130B |
USAF |
|
09-01-1966 |
61-0970 |
C-130B |
USAF |
|
01-02-1966 |
149809 |
KC-130F |
US Marines |
|
19-03-1966 |
61-2641 |
C-130B |
USAF |
|
26-03-1966 |
56-0506 |
C-130A |
USAF |
|
29-03-1966 |
61-0953 |
C-130B |
USAF |
|
15-04-1966 |
10304 |
CC-130E |
Canadian Armed Forces |
|
31-05-1966 |
64-0511 |
C-130E |
USAF |
|
17-06-1966 |
63-7785 |
C-130E |
USAF |
|
..-07-1966 |
24142 |
C-130B |
Pakistan Air Force |
|
06-09-1966 |
63-7878 |
C-130E |
USAF |
|
02-10-1966 |
62-1840 |
C-130E |
USAF |
|
12-10-1966 |
63-7886 |
C-130E |
USAF |
|
25-10-1966 |
61-0955 |
C-130B |
USAF |
|
26-10-1966 |
2452 |
C-130E |
Brazilian Air Force |
|
17-02-1967 |
60-0307 |
C-130B |
USAF |
|
12-03-1967 |
63-7772 |
C-130E |
USAF |
|
16-04-1967 |
58-0722 |
C-130B |
USAF |
|
18-04-1967 |
5-107 |
C-130E |
Iranian Air Force |
|
27-04-1967 |
130309 |
CC-130E |
Canadian Armed Forces |
|
09-06-1967 |
58-0737 |
C-130B |
USAF |
|
17-06-1967 |
60-0293 |
C-130B |
USAF |
|
22-06-1967 |
63-7801 |
C-130E |
USAF |
|
15-07-1967 |
55-0009 |
C-130A |
USAF |
|
15-07-1967 |
62-1815 |
EC-130E |
USAF |
|
08-10-1967 |
61-2649 |
C-130B |
USAF |
|
12-10-1967 |
57-0467 |
C-130A |
USAF |
|
15-10-1967 |
64-0548 |
C-130E |
USAF |
|
15-11-1967 |
62-1865 |
C-130E |
USAF |
|
15-11-1967 |
63-7827 |
C-130E |
USAF |
|
25-11-1967 |
64-0563 |
C-130E-I |
USAF |
|
29-12-1967 |
64-0547 |
C-130E-I |
USAF |
|
10-02-1968 |
149813 |
KC-130F |
US Marines |
|
17-02-1968 |
58-0743 |
C-130B |
USAF |
|
28-02-1968 |
64-0522 |
C-130E |
USAF |
|
02-03-1968 |
56-0549 |
C-130A |
USAF |
|
03-03-1968 |
62-1814 |
C-130E |
USAF |
|
11-04-1968 |
9J-RBX |
L-100 |
ZAC |
|
11-04-1968 |
9J-RCY |
L-100 |
ZAC |
|
16-04-1968 |
56-0480 |
C-130A |
USAF |
|
26-04-1968 |
60-0298 |
C-130B |
USAF |
|
30-04-1968 |
64145 |
L-100 |
Pakistan Air Force |
|
12-05-1968 |
56-0548 |
C-130A |
USAF |
|
12-05-1968 |
60-0297 |
C-130B |
USAF |
|
15-05-1968 |
63-7875 |
C-130E |
USAF |
|
16-05-1968 |
N9267R |
L-100 |
Aerea Aerovias Ecutorianas |
|
22-05-1968 |
56-0477 |
C-130A |
USAF |
|
25-06-1968 |
62-1861 |
C-130E |
USAF |
|
29-06-1968 |
66-0214 |
HC-130P |
USAF |
|
29-06-1968 |
66-0218 |
HC-130P |
USAF |
|
06-09-1968 |
62-1785 |
C-130E |
USAF |
|
19-10-1968 |
64-17949 |
C-130E |
Turkish Air Force |
|
28-11-1968 |
61-2644 |
C-130B |
USAF |
|
| | |