GTinSoCal wrote:
My neighbor growing up was an SR-71 pilot, then later another pilot moved in, a B-1 pilot :-D
2 of my favorite birds!
Now I get to go see her languishing on the ground at the Palmdale Airpark.
"She's only happy going fast"
Col. William 'Hawk' Hawkins, Space Cowboys, 2000
GT
:thumbup: :thumbup: :thumbup: :thumbup: :thumbup:
Here's a few more "fun facts" about the Blackbird that I just found on the Roadrunners website;
SR
-
71 Fun Facts
SR
-
71As
29 operational aircraft built, 11 lost. Trainers built
-
2 SR
-
71Bs, 1 lost & 1 SR
-
71C
Historical
:
54,000 flying hours; 17,000 sorties; 3500 ops missions; 11,000 ops hours; 26,000 refuelin
gs.
1
St
Flt 22 Dec 1964, 1st Combat Flight March 1968, & Operational Flights end Oct 1989
Speed Runs: NY to London 1 hr 5
5 minutes, London to LA 3 hrs 48
minutes
Aircraft 972 arrives Dulles Airport after Speed runs (LA to Dulles 64 min) on 6 Mar 1990
Structure
-
93% titanium
Russian Titanium source
Americas
first stealthy A/C & last designed with
Slide rule
Speed
-
Top speed 3.3 mach, 2,200 Miles/hour, 36 miles/min or 3200feet/sec
Faster than a standard 30.06 hunting rifle bullet when fired.
Normal turn took about 75nm+ radius
Why black?
Prote
ct mostly titanium surfaces &
best heat radiating
col
or to help remove heat from the
aircraft during flight by radiating
heat into the ext
remely cold upper air
-
(
-
55°C/
-
8
0F).
Reduced surface
temperatu
re by up to 50F
at 3.2 mach.
Glass Windows
-
L
aminated Quartz glass a
bout 2.0
inches thick
Average temp
At cruise, about 600°F (causes the aircraft to grow 3
-
4 inches length & 1
-
2 width during
cruise).
Aircraft
Surface
Temp range
from
cool 450 F to hot
engine area 12
00 F. Pilot
pie
windows 620 F
J58 bleed bypass turbojet engines
34,000 lbs thrust in afterburner at sea lev
el; afterburners lit coming off
tanker to initiate climb and acceleration; stay on continuously for cruise until descent 1
-
1/2+ hour
s
later.
6 engine bypass tubes create significant Ram Thrust at higher machs. 83% ram effect at 3.2 Mach.
Engine Chemical Ignition System
TEB (triethylborane), a pyrophoric (burns on contact with air) with
burn temp up to 3000°F.
CORE Engine temperature
-
3400F in Afterburner
Fuel
-
JP
-
7 kerosene base with additives; tanks inerted with nitrogen to prevent auto detonation
Engine oil
70
-
550°F normal temp range; consistency at 60°F honey, 40°F Jell
-
O, 32°F solid. Preheat
engine to 70°F before start.
Tire
s
BF Goodrich, aluminum powder impregnated to reject airframe heat; 425 psi filled with nitrogen; 22
ply rating; 3 ply tread.
Flight duration
-
Most training and ops flights 2.5
-
4.5 hours (required one or two in
-
flight refuelings)
Aerial refueling
-
Airc
raft carries up to 80,000lbs of fuel (12,000+ gallons). Refueling normally lasted
about 12
-
15 minutes with 70,000
-
80,000 lbs of fuel transferred. Normally flown around 25,000 ft with
KC
-
135Q tanker starting at about 325 knots; as fuel transferred from
tanker; it would accelerate to 350
knots IAS (its airspeed limit). Max distance between refuelings about 2800 nm (3200 statute miles).
Pressure
suits
-
Derived from Gemini designs used through mid 70s. Late 70s replacement 1030 pressure
suits would lat
er serve as the initial Space Shuttle
pressure
suits for Shuttle test flights
Cost $250,000
Two Man Crew
(1) Pilot in front with normal flight controls and functions, (2) Reconnaissance Systems
Officer in back had no flight controls; ran astronavigatio
n system, all camera systems, and the aircraft
systems checklist; controlled the electronic defensive systems; and did many of the radio calls.
View at Altitude
-
At 80,000
+
ft you can see the
curvature of the Earth about 350
+
miles in all directions.
The s
ky is a deep blue
-
black, as 97%
of the atmosphere, which gives the blue color, is below.
Engine start
-
Normally 30 minutes prior to takeoff; enough time to do all ground checks and taxi to end
of runway for one final check before taking the runway.
Performance points
-
Most take
-
offs at 40,000 lb fuel load.
From brake release and afterburner light
, about a 4,500 ft takeoff roll in
about 20 seconds.
Liftoff at 210 knots (about 240 mph)
with
Rapid climb passed through 20,000 ft in about 2 minutes.
Afte
r dropping off the tanker and after
burner ignition it took about 17
minutes to climb to 75,000 ft +
and Mach 3. This took about 360 nautical miles distance and consumed 1/3 of your fuel.
Level off normally around 75,000+ ft to a cruise
-
climb condition tha
t, as fuel burned off, would climb
up around 82
-
85,000 ft before starting down
depending on the outside temp & number of turns
.
Descent and deceleration from 80,000+ ft to 25,000ft took about 10 minutes and 220 nm.
Landing approach speed was 175 knots plu
s (200 mph) with landing at 150
-
155 knots (170mph). With
the large orange drag chute the aircraft would stop in about 5000 ft. If the drag chute did not work it
was a 10,000 ft landing roll out to slow and stop the aircraft.
Film and recorders would be d
own loaded for processing after engine shutdown
Buz Carpenter, Smithsonian Udvar Hazy Center Docent and former SR
-
71 Instructor Pilot