Jemiba said:A man in such a rotor chute is nothing else, than with a conventional parachute : A man trying
to save his live. A CSAR heli, although live saving, too, additionally is a measure to save the
fighting power of a soldier. AFAIK that was the rationale, that the RAF began shooting at SAR
aircraft during WW II. With a foldable autogyro/ejection seat there may be the problem, of course,
that an enemy might mistake it for an intentional intruder à la James Bond and then, shooting at him
would be quite ok, without regards, of course of my first point !
GTX said:The Do-335 systemhad some apparently very gruesome results - I think it was one of Captain Eric "Winkle" Brown's book that discussed the results - pilots having arms ripped off etc.
AeroFranz said:GTX said:The Do-335 systemhad some apparently very gruesome results - I think it was one of Captain Eric "Winkle" Brown's book that discussed the results - pilots having arms ripped off etc.
In "Wings of the Luftwaffe" Eric Brown tells of how a couple of test pilots were found in the cockpit with their arms ripped off. Apparently, in order to eject, you had to pull on handles that would release the canopy. Except the handles were part of the canopy itself, so the story goes that if you tried to release the canopy, once the slipstream caught it, your arms would depart with it.
At least that's the "official" version.
hesham said:Hi,
There was anther old escape concept from the 1970s,the Fairchild Model-616
AERCAB aircrew escape rescue capability for combat aircraft,the purpose of
AERCAB was to permit recovery of aircrew who eject from their aircraft over
enemy territory and to provide capability to fly the ejection seat up to 43nm
(50 miles;80 km)at up to 100 knots (115mph;185 km/h) prior to vertical descent
by personal parachute.
Recently revealed by the U.S.A.F. is this escape capsule which was originally designed for the Convair F-102. After the ejection sequence is set into motion the pilot and seat are moved from an upright to a supine position. The pilot can then withstand the 12g ejection loads imposed on him when the capsule is fired from the aeroplane.
INTRODUCTION
The purpose of this program was to provide a rocket catapult
for use in personnel ejection from TRECOM test hover craft vehicles.
These vehicles are fan driven, operating at low altitude.
The scope of the program follows:
(1) Design a rocket catapult for a specific lightweight seat,
the LW-l.*
(2) Conduct tests to assure reliable operation within required
limits of acceleration and rate of onset.
(3) Supply seven rocket catapults for installation in TRECOM
test hover craft.
The XK13 Catapult was developed to meet the ejection needs of
flight crewmen using LW-l seats in experimental flying, platformtype,
U. S. Army vehicles. This catapult is a modified M9 catapult,
and fills the seat propulsion requirements for recovery at zero
altitude and zero velocity.
Low cost was the dominant factor that influenced the design
approach to the XK13 catapult. Components developed and qualified
previously for Air Force catapults were used in its construction.
The modifications were made to provide reduced thrust levels to
both booster and sustainer phases, required because of the weight
of the LW-l seat compared to standard Air Force ejection seats.
This report presents a description of catapult operation, performance
characteristics, and results of testing covducted on the
XM13 catapult.
_____________________
*The LW-l seat is explained in detail in "Ground Operational Recovery
Tests of the LW-I Ejection Seat," TCREC Technical Report 62-47,
June 1962.
Stargazer2006 said:Some early 1950s Lockheed escape concepts:
Zeppelin said:- ejection seats for passenger planes !!
Great way to get rid of a bunch of rowdy passengers!bigvlada said:The whole passenger section, from cockpit to the rear end would be jettisoned