RTV-G-4 Bumper

  (Redirected from Bumper (rocket))

The RTV-G-4 Bumper was a sounding rocket built by the United States. A combination of the German V-2 rocket and the WAC Corporal sounding rocket, it was used to study problems pertaining to two-stage high-speed rockets. The Bumper program launched eight rockets between May 13, 1948, to July 29, 1950.[1] The first six flights were conducted at the White Sands Missile Range, the seventh launch, Bumper 8 on July 24, 1950, was the first rocket launched from Cape Canaveral.[2]

Bumper
Bumper.jpg
Bumper 5, launched February 24, 1949
FunctionSounding rocket
ManufacturerArmy Ballistic Missile Agency
Country of originGermany/United States
Size
Height62 feet (19 m)
Diameter5 feet 5 inches (1.65 m)
Launch history
StatusRetired
Launch sites
Total launches8
First flightMay 13, 1948
Last flightJuly 29, 1950
First stage - V-2 rocket
Thrust27,200 kgf (267,000 N; 60,000 lbf)
Burn time60s
Propellant
Second stage Wac Corporal
Thrust6.7 kN
Burn time47s
PropellantAerojet liquid-fuel

Bumper programEdit

BackgroundEdit

 
Bumper in two pieces: V-2 first stage behind WAC Corporal second stage

The Bumper program to produce and launch a two-stage combination of the V-2 and WAC Corporal rockets was conceived in July 1946 by Colonel Holger N. Toftoy.[3] Both the WAC Corporal and the V-2 had been extensively tested at White Sands Proving Grounds, the WAC Corporal's launch series occurring in late 1945/early 1946 and the V-2 launches beginning March 15, 1946.[4]:235–237

Bumper was started on June 20, 1947, to:

  • Investigate launching techniques for a two-stage missile and separation of the two stages at high velocity.
  • Conduct limited investigation of high-speed high-altitude phenomena.
  • Attain record-setting velocities and altitudes.[2]

Bumper employed the V-2 as first stage and the WAC Corporal as second stage. In a typical flight, the V-2 engine would fire first, taking the Bumper combination to an altitude of 20 mi (32 km), at which point the WAC Corporal would be released under its own power. This separation occurred before V-2 Brennschluss (engine cutoff) to ensure that the WAC Corporal had a stable, actively controlled platform to lift off from, and also so that the V-2 would impart close to maximum possible speed to the Bumper's second stage. The V-2 rocket had a maximum altitude of around 100 mi (160 km), while the WAC Corporal without it's solid rocket booster, had a theoretical maximum altitude of 25 mi (40 km) (43.5 mi (70.0 km) with). Together, Bumper could reach altitudes of more than twice those attainable by the V-2 alone.[4]:235, 260

Engineering and limited scientific results (for instance, air resistance at high altitude)[4]:259 would be obtained from the 25 lb (11 kg) telemetry payload carried by the WAC Corporal second stage.[5] Though the Bumper program was not, itself, a secret, aspects of it were classified, particularly the way the WAC Corporal was fitted into the nose of the V-2.[6]

PlanningEdit

Overall responsibility for the Bumper program was given to the General Electric Company and was included in the Hermes project. The Jet Propulsion Laboratory was assigned to perform the theoretical investigations required, design the second stage, and create the basic design of the separation system. The Douglas Aircraft Company was assigned to fabricate the second stage, and do detailed design and fabrication of the special V-2 rocket parts required.[2]

No German engineers were directly involved with Project Bumper, though some worked on the initial studies regarding the mating of the V-2 and WAC corporal. Two women, Mary Taggard and Bea Sylvester, were on the Bumper team providing rocket (but not launch) support.[6]

OperationsEdit

Six Bumper launches were made from White Sands Proving Grounds. The first four, launched in 1947/48 were test flights of varying degrees of success.[1] The first fully successful Bumper flight was the fifth in the series, launched at 3:14 P.M. (MST), February 24, 1949.[4]:257

Bumper 5 was the first in the Bumper series to be launched with a fully fueled second stage.[1]. One minute after blast-off, at an altitude of 20 mi (32 km) and a speed of just under 1 mi (1.6 km) per second, the WAC Corporal detached from the V-2 first stage and fired its own engine. Forty seconds later, at second stage Brennschluss, the WAC Corporal had reached its maximum speed of 1.39 mi (2.24 km) per second.[4]:257 It reached its peak altitude of 250 mi (400 km), a world record[7], six and a half minutes after launch.

The V-2 first stage crashed into the New Mexico desert five minutes after launch 20 mi (32 km) north of its firing site. The WAC Corporal hit the ground 12 minutes after take-off 80 mi (130 km) from its launch pad. So great was its velocity upon impact, higher than any rocket to date, that the wreck was not found for analysis until January 1950.[4]:257–8

In 1949, the Joint Long Range Proving Ground was established at Cape Canaveral Air Force Station on the east coast of Florida, where the last two Bumper launches would take place. On July 24, 1950, Bumper 8 became the inaugural launch of "the Cape", still in use as of 2021.[2] Both Bumpers 8 and 7 (fired in that sequence, a week apart) were fully successful low-angle launches designed to maximize range (~200 mi (320 km)) rather than altitude.[4]:259. These flights were much ballyhooed in the American press.[5]

Launch historyEdit

Rocket number Time Launch site Pad Maximum altitude Remarks Image
1948
Bumper 1 May 13, 1948 White Sands Pad 33 127.3 km (79.1 mi) Test flight; WAC 2nd stage partially fueled.
Bumper 2 August 19, 1948 White Sands Pad 33 13.4 km (8.3 mi) First stage failed due to propellant flow interruption.
Bumper 3 September 30, 1948 White Sands Pad 33 150.3 km (93.4 mi) WAC stage failed.
Bumper 4 November 1, 1948 White Sands Pad 33 4.8 km (3.0 mi) Explosion in tail of V-2.
1949
Bumper 5 February 24, 1949 White Sands Pad 33 403 km (250 mi) Successful flight. Separation of stages at 35 km (22 mi).  
Bumper 6 April 21, 1949 White Sands Pad 33 49.9 km (31.0 mi) Premature V-2 cut-off; WAC stage failed to fire.
1950
Bumper 8 July 24, 1950 Cape Canaveral Pad 3 16.1 km (10.0 mi) Low-angle atmospheric flight over 320 km (200 mi) range. First rocket launch from Cape Canaveral.  
Bumper 7 July 29, 1950 Cape Canaveral 16.1 km (10.0 mi) Low-angle atmospheric flight over 320 km (200 mi) range.  

[1]

See alsoEdit

Spaceflight before 1951

ReferencesEdit

  1. ^ a b c d "Bumper Project". White Sands History – Fact Sheets and Articles. US Army. Archived from the original on 2008-01-10. Retrieved 2007-12-02.
  2. ^ a b c d "A Brief History of Rocketry". History of Manned Spaceflight. Merritt Island, Florida: Kennedy Space Center. 2000-08-24. Archived from the original on 2009-01-07. Retrieved 2008-10-01.
  3. ^ "Biographies of Aerospace Officials and Policymakers, T-Z". NASA History Division. Retrieved 2012-07-01.
  4. ^ a b c d e f g Willy Ley (June 1951). Rockets, Missiles, and Space Travel. Dominion of Canada: Viking Press. OCLC 716327624.
  5. ^ a b "Overselling the Missile". Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. 1950-07-31. p. 46. Retrieved 2021-06-19.
  6. ^ a b "Bumper: The Story Behind the First Launches From the Cape". NASA. 2007-11-22. Retrieved 2021-06-19.
  7. ^ "'Bumper' Missile in Public Showing". Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. 1950-07-24. p. 17. Retrieved 2021-06-19.