One of the requests that Diane made when I started doing monthly articles for her was to cover space related projects. This was because our sector includes the former TRW, which has an incredible space history.
Fortunately, I also had a strong interest in that subject, so the request was not a hard one to fulfill. I am, after all, a child of the space age. But I remain a heritage Northrop guy and even though I greatly appreciate the history of Grumman, Ryan, Radioplane, TRW and Scaled Composites, any chance I get to explore Northrop legacy programs and proposals I will do so in a heartbeat.
This is not to say I won't explore the other heritage companies' histories - I have and I will continue to do so and they will eventually be posted here. But availability is also a key and I have had much more success with finding Northrop history than with the other companies, save perhaps Ryan.
The Mercury Program is of special signifcance to me. I remember my mother waking me in the early morning to watch Alan Shepard's suborbital flight and later John Glenn's launch and three-orbits around the Earth. Nearly twenty years later the circle would close as I roused my six-year old daughter to watch Columbia make the maiden voyage of the shuttle program into space. Perhaps someday she can watch a launch to Mars with her kids in the wee hours of the morning.
One final note: I did manage to find some information on the Grumman G-214, their Mercury proposal. Be on the lookout for it in the next few days.
This article was originally published in the Northrop Grumman Engineering Department in-house, on-line magazine Airspace, vol. 2, no. 6, in April 2011. It is re-posted here with permission and has approved for public release case number 12-1474.
Chasing Mercury – The Northrop N-227
By Tony Chong
April 12, 2011 marked the 50th anniversary of the
launch of Vostok 1. On that day in 1961
Soviet cosmonaut Yuri Gagarin became the first human to go into space. He also became the first human to orbit the
Earth.
Twenty-three days later, on May 5, 1961, Alan Shepard became
the first American astronaut to go into space during a 15 minute, 28 second
sub-orbital flight that took him 303 miles downrange from the launch site at Cape
Canaveral, Florida. Shepard rode inside a
Mercury capsule fitted to a U.S. Army Redstone missile.
Project Mercury, America’s first series of manned
spacecraft, was a program designed to put an American into space as quickly as
possible. It was not, however, a hastily
conceived stop-gap measure. In actuality
the ballistic manned satellite concept was one of three methods under active
consideration by the U.S. Air Force since 1956 for establishing an American presence
in space, with the initial phase eventually being called “Man In Space Soonest”
and the fourth and last phase to encompass a manned lunar landing fifteen years
after program start.
Sputnik’s launch on October 4, 1957 changed all of the
dynamics in the blossoming American space program. Faced with a need to respond to the Soviet
initiative, and with a desire to curb military expansion into space, President Dwight
Eisenhower threw his weight behind a civilian-controlled agency. The important, but obscure National Advisory
Committee for Aeronautics was remade into the National Aeronautics and Space
Administration, effective October 1, 1958.
NACA had itself examined the three basic types of manned
spacecraft – ballistic, skip and glide – prior to Sputnik. For a variety of good reasons (launcher
capabilities and developmental issues, among others), the new NASA chose the
ballistic approach. McDonnell Aircraft Corporation
won the competition to build the capsule, but what is largely forgotten is that
heritage Northrop Aircraft, Inc. competed for that program as well.
Northrop was one of the eleven aircraft manufacturers that
responded to the Air Force’s 1956 request to industry for manned satellite
concepts. As late as January 1958 the
company (which changed its name to Northrop Corporation on February 2, 1959) adhered
to the more sophisticated “boost-glide” vehicle proposal, the basis for the
eventual X-20 Dyna-Soar (Dynamic Soarer) program won by Boeing in June 1959. However, with NASA issuing a specification on
November 14, 1958, for a ballistic capsule, Northrop answered with a design
that carried the internal designation N-227.
NASA’s specifications included the need to fit the capsule
to both the Redstone missile (for sub-orbital flights) and the Air Force/Convair
Astronautics Atlas missile (for orbital missions). Additional requirements for a launch-escape
rocket tower system, a retro-rocket system for de-orbiting, a zero-lift body
utilizing blunt-end re-entry for drag braking, pilot controllability of the
capsule and the ability to land in water also drove the basic shape of the
design.
Northrop’s proposal was very similar to the winning McDonnell
vehicle. The main visual differences
were in the wider diameter at the blunt end for the Northrop craft – 80 inches
versus McDonnell’s 74.5 inches – and the shape of the forebody of the
capsule.
The launch-escape rocket tower structure also differed in
where it attached to the two proposals.
Northrop’s craft featured a constant-diameter forebody with the tower
joined to the flat end (top) of the vehicle.
McDonnell’s design had a tiered forebody with the tower structure fitted
over the smaller diameter upper section.
Both designs also featured a corrugated look to the capsule
exterior surface. However, Northrop’s
corrugations ran along the length of the vehicle while McDonnell’s formed
around the circumference of the craft.
Final designs on this fast-tracked proposal were due by
December 11, 1958. The NASA selection
team worked over the Christmas holidays to determine the winner. Northrop did not make the final cut.
Ironically, heritage Grumman, a late entry into the manned
spaceflight game, did. It essentially
tied with McDonnell as having the best design.
However, because Grumman was deemed to be short on manpower due to some impending
Navy contracts, the award was given to McDonnell on January 12, 1959.
Alan Shepard would make his historic flight just two years
and four months later.
Kristi Harding of Records Management contributed to this
article.
Any information on the Grumman Mercury proposal would be
greatly appreciated by the author for incorporation in a possible future
article.
For further reading, check out “This New Ocean – A History
of Project Mercury” by Swenson, Grimwood and Alexander, NASA SP-4201 in the
NASA Historical Series, U.S. Government Printing Office, 1966.
For “Man-In-Space-Soonest” background information, check
out: http://www.astronautix.com/fam/manonest.htm
On-line information on Project Mercury can be found at: http://www-pao.ksc.nasa.gov/history/mercury/mercury.htm
and http://www.thespacereview.com/article/586/1
Tony Chong is a
historian, photographer and a contributing editor to Airspace. He leads
activities in the Aerospace Systems Display Model Shop and works in El Segundo.
Photo Captions
1) N-227 3-view: This 3-view
drawing taken from the Northrop proposal shows the basic layout of the
N-227 design. Note the shape of the
forebody, the attachment of the launch-escape rocket tower and the
diameter of the blunt end of the spacecraft. The head-on view shows the linear
corrugations on the skin. Photo credit: Tony Chong collection
2) McDonnell
3-view: By comparison this general arrangement 3-view drawing of the
McDonnell capsule, taken from one of its proposal pages, shows a tiered
forebody, a narrower diameter in the widest part of the capsule proper
(the adapter shroud flares out more) and a different method of attaching
the tower structure to the spacecraft.
Photo credit: Tony Chong
collection
3) N-227
stats: Another page from the Northrop proposal features a weights and
balance breakdown of the various components of the company’s design. Photo
credit: Tony Chong collection
4) img066: Northrop’s
proposal featured an artist’s concept painting of the N-227 in the
splashdown/recovery phase. The
linear corrugations show up well in this interpretation, as does the inflated
orange, torus-shaped landing impact airbag with an internally-fitted stabilization
water bag. The artist’s signature
says “Todd.” Photo credit: Tony Chong collection
5) 158209:
Several photos were taken of a small model of the N-227 showing how it
would have looked mounted on a Redstone or Atlas missile. This particular image shows the rather
ungainly looking transition fairing and how it would have joined to the
Redstone missile. Photo credit: Northrop Grumman
6) mr-2: Contrast
the previous image with this of the McDonnell Mercury capsule fitted to
the Redstone missile. Even with the
slight overhang, the smaller diameter of the McDonnell design makes for a
much cleaner fit to the launcher. Photo credit: NASA
7) 158208: This image shows the model of the N-227 separated from
the Redstone launcher. The combined
fairing, capsule and launch-escape rocket tower assembly sitting next to
the Redstone body gives a good indication of the relatively small size of
the missile, as if emphasizing that it was only powerful enough for sub-orbital
flights. Photo credit: Northrop Grumman
8) 158206: The fairing on the
N-227 and how it joins to the Atlas missile is shown in this photo. Note the inverse taper from the
capsule’s 80” diameter body to the smaller diameter top of the Atlas. Photo
credit: Northrop Grumman
9) GPN-2003-00042w:
Again, the contrast between the Northrop proposal and the actual
Mercury/Atlas combination is noticeable.
While still featuring an inverse taper, the McDonnell fairing is
much shorter than the N-227’s. An
obvious question would be did the taller fairing and wider capsule, with
perhaps its potential vibration and/or stability problems along the
transition structure, play a part in Northrop’s loss? Photo
credit: NASA
10) 158207:
The N-227, with its tower and fairing, is shown separated from the
Atlas booster. The hand is a good
indicator of the size and scale of the model. Photo
credit: Northrop Grumman
Cool, Tony. Thanks.
ReplyDelete...Outstanding work, Tony! On a side note, the comments about the adapters does beg the question: who was/would have been responsible for the final design and construction of those adapter(s)? The spacecraft manufacturer, or the booster manufacturer?
ReplyDeleteIn the case of the Mercury Program it was McDonnell that developed the adapter. It appears McDonnell may have subcontracted out the adapter on the Gemini Program, but I am not certain of that. I have not delved into the Apollo Program yet, so I can't answer for that case. Based on this I would assume Northrop would have been responsible for the adapter on their Mercury version.
DeleteJust found this site after watching one of Tony's excellent lectures on Northrop for the Torrance Museum.
ReplyDeleteIt is interesting that Boeing have had issues with the design of the adapter section between the Atlas 5 rocket and their CST 100 /Starliner capsule.
Old problems keep resurfacing.