NASA Johnson Space Center
Oral History Project
Edited Oral History Transcript
Joseph
F. Shea
Interviewed by Michelle Kelly
Weston,
Massachusetts –
26 August 1998
[The
following interview of Dr. Joseph Shea was conducted in Weston, Massachusetts
by Michelle Kelly on August 26, 1998.]
Kelly:
How did the LOR [Lunar Orbit Rendezvous] decision come about? I know
Mr. [John C.] Houbolt wrote his paper and presented it to the various
people within NASA, but how did they really take notice of the paper
itself as a different approach?
Shea: … [Dr. [Robert C.] Seamans
gave a copy of Houbolt’s letter to [D.] Brainerd Holmes. Holmes
put the letter from Houbolt and Seamans] on my desk and said, "Figure
it out." The tail end of this [letter] talks about LOR and [we]
decided all we would do would be to study direct flight versus LOR
and not anything else.
Houbolt played no part in this [study] at all. Houbolt was an apostle.
Just read [the letter] those papers, you'll see how he was complaining
about how the studies went, and they weren't fair, and all this sort
of stuff, all this junk.
Kelly: Can you tell me a little bit
about how you managed the different centers from headquarters, and
just a little bit more about what you had just spoke earlier, about
giving some of the different centers some of the opposing positions
of which to study?
Shea: I could tell them, "Will
you guys please study this and please study that?" The centers
did not work for us; they worked for Seamans [Robert C. Seamans, Jr.],
but they did respond to a certain amount of direction.
Kelly: Did you come up with your own
philosophy about how to do that, or was it just whatever you thought
best?
Shea: I just did it. When you run programs,
you know how to run programs.
Kelly: Well, it very much seems to me,
even from what other people have said with respect to your management
style, I heard you basically wrote the book about managing large-scale
technology and technological programs in the aerospace industry.
Shea: Well, I don't know about that.
Kelly: A lot of people have said, not
just one.
Shea: See, you had to force it down
to things that were either quantitative or sufficiently qualitative,
and there were a number of qualitative things. For instance, in a
direct flight mode, which was what Werner [von Braun] was interested
in, the idea was that the whole command and service module was going
to land on the moon. Well, when you really looked at that, that's
what these meetings were, the big meetings: "Tell me how we're
going to do this in detail." I've got the service module engine,
with a bell underneath it. [Drawing] Okay, so here's the command module,
the service module with the fuel and the fuel cells and all that sort
of stuff, then an engine. Now, here's the lunar surface. It's got
rocks, it's got dust, it's got junk all over the place. These are
all going to be kicked up. Now, I can't land [the CSM [Command and
Service Module] on the lunar surface], because I have to use [the
Service Module] to take off on, so I have to somehow come up with
a landing gear of some kind, not unlike what the lunar module actually
finally had.
But now that had to be added to the service module, so the service
module is no longer the simple thing that Houston was thinking it
was; it was getting more complex. As a matter of fact, it probably
needed—I couldn't have this engine built too close to the surface,
or I might damage the engine when it was taking off, so it would have
been better if this lower part of this thing was more like a solid
piece. So it's no longer just a single service module. And that's
when NASA, in its way of sharing the wealth among the centers, [Abe]
Silverstein was running Lewis [Research Center], the propulsion center,
and it was sort of semi-decided … that Silverstein would do
this. So he had a vested interest now in the program.
So I called Silverstein in just like I did with Werner, went through
the thing with him, showed him how complicated this really was and
how much more it was going to cost. Silverstein was a rough old bastard,
though. I finished the briefing, he said to me, "That is the
most dishonest technical briefing I have ever heard." Tough.
But the reason he said it was because it cut him out of a piece of
work for his center. Those centers were so used to competing with
each other for resources and trying to make themselves as big as they
could be, they were parochial, is the appropriate word. The fact that
this had to be added in, it came out of these two big meetings I had,
one on how do we do Earth orbit rendezvous or direct flight, and how
do we do the lunar orbit rendezvous. That was that.
Kelly: This was in 1962 once the decision
was made?
Shea: Yes.
Kelly: What happened after that decision?
What did you go onto after? I believe it's my understanding you were
still working at headquarters with Mr. [D. Brainerd] Holmes.
Shea: Yes, but Holmes didn't last long
at headquarters. I was writing the system specifications and trying
to put order into what were the priorities in the program… Safety
was …, the most important. Second was probably schedule because
of the end of the decade. Third was—I'll give you another little
something you can have.
Kelly: Thank you. What types of things
do you think of as far as writing specifications for something that
has never been done before?
Shea: Well, it's relatively simple,
as a matter of fact.
Kelly: Can you tell me a little bit
about it?
Shea: Well, obviously we had to be safe,
and obviously we had to put a man on the moon and come back. So, safety
had to be, we thought, or I thought, [balanced] against mission success,
but they both had to be important. So the first specs I wrote said
that safety had to be .999; in other words, one chance in a thousand
of losing the astronauts. Mission success had to be about 90 percent.
You could afford to do it if you got there one time out of ten.
I then tried to translate that into reliability requirements on all
of the system elements, and then the actual studies that we ran broke
the various modes down into maybe a hundred different steps: start
this engine, stop this engine, stage, do this, do that, the other
thing, assign a nominal probability to each of those [events] the
way you calculate the probability of a whole bunch of things, and
the [process] is to multiply it altogether, and then you come out
with a number that tells you. As long as you have used the same numbers
for the same step in each of the two missions you're comparing, then
you can make a valid comparison. So the first numbers came out like
30 percent probability of mission success, which was optimistic, and
about a little less than one chance in a hundred of losing the astronauts.
That's about all you can expect in terms of accuracy, those kind of
studies.
Kelly: Were those just random numbers
that you had picked, or was there a basis for them?
Shea: Try and put it any higher, you
can't ever prove it. There is an equation, in fact, when you read
Logasen's paper, you'll see something about the Large Launch Vehicle
Planning Committee, which was a joint DOD [Department of Defense]—Large
Launch Vehicle Planning Committee, which had Nick [Nicholas E.] Golovin
[as chairman]. He estimated that before he would be willing to put
a man on top of a Saturn V, he would need something like 95 percent
assurance of 90 percent reliability. In other words, one launch out
of ten might fail, but he'd like to have 95 percent [assurance]. The
equation for that is, if I tested N times to try and get the reliability
assurance, is R to the Nth reliability I'm looking for, 90 percent
to the Nth equals one minus .95. Work that equation out, and N equals
forty-eight. So I have to launch forty-eight unmanned Saturn Vs, which
I couldn't [afford]. I could only launch one about every three months
at the most. The program would have been still going on.
So we finally concluded there was no way to assure statistical reliability.
You had to really use engineering confidence and do a little wishing
and lucking and hoping.
Kelly: And the Saturn V hadn't really
been testing all that much before it was actually launched with men
on top of it.
Shea: Well, actually, we went away from
what had been the more traditional kind of testing, which I would
call incremental testing, to what was called all-up testing. Now,
see if you can catch this on tape, because it is important.
Kelly: Okay.
Shea: The way the Germans, in particular,
like to test rockets, Saturn V is a three-stage rocket. Okay? So they
would like to test several first-stage only, with just dummy second
stages, then test first-stage and the dummy second stage, and then
finally test the whole rocket. Okay? So you were just barely getting
started. Now, this was the way we had started in the [Air Force] Ballistic
Missile Program, too. We found every time we added an extra stage,
by the time we got it integrated at the Cape, it was just as much
trouble as starting a new launch vehicle.
Now, I should go back and make a point …, that [is] the program
philosophy. That [is] very important for a program to have a philosophy.
The program philosophy came out of three sources: the von Braun German
team, the NACA aerodynamicists, and the few of us like George [E.]
Mueller and myself, who had worked on the Air Force ballistic missile
program. So it was the synthesis of those three philosophies. And
we decided this incremental approach didn't make any sense at all,
that what we would do would be to go to "all up." In other
words, [on the first launch, all stages] would be a real stage…
If [the first] one works, by God, you're now ready to [ignite and]
test the second stage. You're ahead of the game already. [If second
stage] one works, you can test the third stage and you're ahead of
the game again. There's no need to do it incrementally. So that was
really the origin of the "all up" philosophy.
The second part of it was, it saves a lot of schedule time, because
every launch we took out was saving three months, and the rest of
the schedule was slipping anyhow, and we could still hold in the first
manned flight date, because we could sort of adjust the schedule.
So "all up" was the decision that enabled Apollo to get
to the moon on time.
The first schedules had about ten [incremental vehicle tests] in them.
We finally cut it down to two. The philosophy we used—this was
Mueller and myself mostly—"We'll shoot one all up, put
a lot of heavy telemetry on. If everything works, we're ahead of the
game. We're going to shoot a second one to make sure the first one
was not a random success." You talk about random failures. You've
got to have random successes. "So you shoot a second one, and
again, if everything works all right, then we will put men or a spacecraft
aboard a third." That's the whole genesis of the so-called "all
up" philosophy, which you may or may not have heard about.
Kelly: I have, as a matter of fact.
Who came up with that idea? How did that idea evolve?
Shea: Well, it first happened when Holmes
was still there and the schedule has slipped. We had, I think, ten
launches scheduled. I went to Brainerd, "Look, we're not statistically
significant anyhow. Why don't we take out three or four launches?
You'll gain back a year, and you'll be back on schedule." So
[he] agreed to that.
Then when Mueller came in, he understood this better, so he and I
worked this out together. I can't say it was his idea, I can't say
it was my idea. It was just the two of us. Selling it to Werner was
not easy, but we sold it to Werner.
Kelly: How did that come about?
Shea: We just told him that's the way
it's going to be, finally. By that time we were in stronger control
of the program, because we finally had [agreement on] a clear mode
to go, and the program was on its way. It was gaining momentum, and
it's a little easier to get people to go along with you when you're
gaining momentum.
Kelly: When was this decided that you
would go ahead with the "all up" testing as opposed to the
incremental testing?
Shea: That would have been shortly after
Mueller came in, probably within six months of Mueller coming in.
You'll have those dates someplace.
Kelly: Sure. It seems like NASA's still
using this philosophy.
Shea: Yes, of course. So's the Air Force.
That's what makes sense.
Kelly: It saves money and saves resources.
Shea: And the important thing is, if
[the stages at testing] this works, I will take advantage of its working
by finding out whether this one works, and again, I'll find out if
… in one launch I can evaluate my whole stack, instead of requiring
three or four or five launches to have a chance of evaluating the
whole stack.
Kelly: While you worked on both the
Titan I and Titan II programs, did you have similar philosophies,
or were you not necessarily involved in the entire program [unclear]?
Shea: I was involved in the entire programs.
Kelly: Can you tell me a little bit
about how that worked with actually designing the Titan, and developing
it and testing it?
Shea: No, I was the system engineer
on the guidance system for Titan. That was a radio system, involved
a radar that was derived from the Nike Hercules. I was the one that
had to figure out how to take our equipment and integrate it into
the missile. So I was the main interface between Bell Labs in New
Jersey and the Air Force and TRW and the air-frame people on the West
Coast. I could not have had a better learning experience. I learned
how engines worked, how power systems worked. I went through everything
that you had to do to get systems integrated together into a missile.
Then when … I ran the [Titan II] Guidance Program, that gave
me the management experience of actually running the whole program.
Kelly: When you were involved with the
Titan Project, did you have any idea that it would be sending men
into space at the time that you were actually integrating the programs,
the systems?
Shea: No, it was strictly a ballistic
missile at that point in time.
Kelly: Were you involved at all, or
did you even hear about the decision to use it within the manned space
flight program? The Titan II, I believe, then it was.
Shea: That came later on. That's much
too small a vehicle. That only puts 40,000 pounds [in orbit], much
too small a vehicle. I did not get involved in that.
Kelly: So you just jumped right on into
Apollo then.
Shea: Yes, essentially I went from Titan
to Apollo, yes.
Kelly: Were you involved at all in the
selection of the contractor to build either the Saturn V—I know
that there were several various contractors.
Shea: No.
Kelly: Or the command module itself?
Shea: No. That was done by the centers.
Kelly: It was done by the individual
centers themselves?
Shea: Yes.
Kelly: Were you at that time working
with them at all while you were at headquarters, or you just oversaw
what the centers did?
Shea: Just oversaw. We did not get involved
in the source selection, if that's what you're asking.
Kelly: Okay. That makes sense. Was there
anything else that you'd like to talk about with respect to your time
at headquarters? Because I'd certainly like to talk to you about your
time at the Manned Spacecraft Center, but I don't know if there might
be anything in addition you'd like to add.
Shea: Well, I would almost say—let's
save the time at the Manned Spacecraft Center [for later], because
that involves a different role. That involves the actual role of managing
the program.
Kelly: Right.
Shea: It's a long story. I found a mess
when I went to Houston, and even a bigger mess equivalently than the
system engineering mess that I found at headquarters.
Kelly: How did you get involved in fixing
these problems, or in determining what these problems were?
Shea: You want an example?
Kelly: Sure.
Shea: I'll give you a simple example.
Do you know what a specification tree is?
Kelly: Yes.
Shea: All right. So when you lay your
program out, you have your top spec, and then you come down from the
top spec, and you go to each of the boxes, and you say what the requirement
in the box has to be, you say what the cost should be, we estimate
what the cost could be, and then you hopefully set a schedule for
it. Well, I'd been at Houston running the program for, oh, more than
six months, been there probably a year.
The one thing I did when I went to Houston that was different than
the way they had been managing. The guy who was the program manager
first was a guy named Charlie [Charles W.] Frick, who was a terrible
program manager. He kept the program office isolated from the rest
of the center. But the rest of the center had, say, a thousand people,
and he had a hundred. I knew that the thousand people they all worked
for [Maxime A.] Faget, and they had access to contractors. They could
go and look and see what the contractor was doing, comment on it.
In principle, they shouldn't give direction and say, "Do it this
way," but they did anyhow. So it was very hard to keep any kind
of contract control on. And they had no other responsibility. So I
took all of the systems specs and turned them into—do you know
what a work package is?
Kelly: No, sir, I don't.
Shea: Well, take the systems spec that
you've gotten from the spec tree, and the cost estimate, how many
man-months per month you're going to have to spend on it, and how
much material, what sort of schedule or milestones you're looking
for. We made those into individual contract packages which we then
gave to the individuals in Faget's organization as their responsibility.
So they had to report to me, not just on technical progress, but on
cost progress and schedule progress. I set up a scheme of having [them]
write me a memo once a week to tell me where their organization was,
and I would annotate the memo, send it back, and we'd annotate it
back and forth, or work the problems out.
So the one example I would give you is, we finally got equipment enough
to test the heat shield material. The heat shield, if it stays in
one attitude and the sun is beating on it from this side, the temperature
goes to about plus-250 degrees Fahrenheit. The other side, which is
now looking at outer space, which is cold, so it's radiating in outer
space, and it goes to about minus-200 degrees Fahrenheit.
So we finally got the ability to put the heat shield material in an
electric shock tube, heat it up to 250 degrees, and then cool it down
to see what would happen. The surface of the material started to crack
and craze, and the heat shield guys came to me and said, "Oh,
we've got to start a whole new heat shield program. Estimate $60 million;
we can't tell you the time."
So I scratched my head and I said, "How long does it take for
the temperature to change from, let's say, ambient temperature to
this minus-200 or plus-200?" It's called a time constant.
"Oh, about thirteen hours."
I said, "[Why] the hell does the spacecraft have to stay in any
given attitude for thirteen hours?" It's a three-day trip to
the moon, and three if you're back, but I can certainly change the
attitude. You know, the idea of just slowly rotating the spacecraft
one revolution per minute.
Well, the medical people said, "Oh, the astronauts [might] get
dizzy…”
The attitude control people said, "Well, we're not sure whether
the attitude and control [system can keep it stable]."
Well, I knew enough about control systems, and I knew they could do
that. So I sent them back to the drawing board, and we put the rotisserie
mode in, so we slowly rotated going up to the moon, and slowly rotated
to come back again. The temperatures never varied more than about
40 degrees plus or minus on the heat shield. That's what a program
manager can do, ask the fundamental question, "Why is the requirement
what the requirement is? Does it make any sense, and how can you change
it, or can you change it safely without any problem?"
Same thing happened on the docking mechanism. The structure people
came to me who designed the docking mechanism, "Oh, we can't
make it strong enough for the LM to push the command module."
I said, "Oh, come on, you know you can do that. It's easy enough
to do."
Well, it's more [an attitude] control system problem which they could
solve. So I insisted that as part of the redundancy, because the only
two non-redundant elements aboard the spacecraft are the engines on
the lunar module and the engines on the service module. So I insisted
that the [lunar] module be able to control and push, that the interface
be strong enough that they be able to push the command module. If
it hadn't been for that decision, the movie Apollo 13 would have been
a tragedy instead of fun. But you've got to ask the right question
and you've got to understand the system. That's all.
Kelly: That's interesting. You had mentioned
that the only two systems that weren't redundant were the engines
on both the command module, or service module, and on the LM. Were
you involved in making that decision?
Shea: There was no other way to do it.
You couldn't put two engines on. We made all the valving and piping
and everything else … redundant. The only thing that wasn't
redundant was the engine bell itself. That was something we decided
we could live with, so we did.
Kelly: What other types of things did
you work in with respect to getting the command module along the lines
and getting it moving forward to the point where they could actually
use it as a spacecraft?
Shea: Well, you could always use it
as a spacecraft. It was designed as a spacecraft. It came out of a
study that had been done by the space task group long before Apollo
started. It was designed to be a three-man spacecraft, and it was
an adequate three-man spacecraft.
Kelly: How did it go from the drawing
board onto the actual assembly line and actually producing them? Can
you tell me a little bit about some of the decisions that were made?
For instance, I'll just think of an example. Some of the systems with
regard to the environmental control system, or the reaction control
system.
Shea: Those were easy systems to spec.
The thing I found when I got to Houston was that there were a number
of test spacecraft, and North American was making every goddamned
one of them different by a little bit as the design was evolving.
I said, "That's too expensive. We're going to stop that. We're
going to have one block, one design, until we get the lunar module
designed, and then we'll have a combined design for the lunar module
and for the command module. That'll be called block two." And
that was what finally flew.
Kelly: Why didn't the block one command
module ever fly?
Shea: Because it burned up.
Kelly: That was the only one that was
designed, then?
Shea: There was one more.
Kelly: Can you tell me a little bit
about working with North American? I had heard from several other
people that I've interviewed that they had been working with McDonnell
for so long during the Mercury and Gemini Programs that the really
felt comfortable with them, but it was just a very different atmosphere
working with North American.
Shea: North American was a very difficult
company to work with. The night they won the contract for the [unclear]
service module, they had a party. They gave out hats, [unclear] hats.
Do you know what was on the hat?
Kelly: What's that?
Shea: Here's what the hat looked like.
[Drawing: NA$A]
Kelly: Oh, no.
Shea: Yes, ma'am. That's right. Honest
to God, that's how—
Kelly: Just for the tape I'm going to
say that it says NASA with a dollar sign as the S (NA$A).
Shea: Dollar sign in the middle. And
they acted that way most of the time.
Kelly: Oh, really? Had you ever worked
with any of the people at North American before?
Shea: No.
Kelly: So it was a totally new ball
game for you, then.
Shea: Yes.
Kelly: Can you tell me a little bit
about your first introduction with North American and the relationship
between NASA and North American?
Shea: Well, I wrote a memo to George,
one of which I will give you next time.
Kelly: Okay.
Shea: We cited some eleven or twelve
conditions under which I would go down to Houston and take over the
spacecraft program job. It involved changing out people; it involved
a few changes in system philosophy. We can talk about that next time.
Kelly: Okay. I'm very interested to
find out how you got to Houston and why they asked you to go.
Shea: Because after Frick quit, Bob
[Robert O.] Piland, who had been his deputy, became program manager.
Piland didn't want to be program manager. Mueller came in. Piland
quit after Mueller came in. I sort of hinted to Mueller that I would
be willing to go down to Houston and run the program if he wanted
me to. Then I wrote him a memo which essentially contained the conditions.
[unclear].
Kelly: Thank you. This is your memo
to Dr. Mueller.
Shea: You might want to write on top
of that, "Conditions for going to Houston."
Kelly: Okay. I'll jot this down here.
Did you then go to MSC shortly after that and then Spacecraft Center
after you discussed this?
Shea: Yes. Almost immediately.
Kelly: Oh, really? What was that like
uprooting your family and going to Houston?
Shea: They were used to being uprooted,
poor kids.
Kelly: What was the Manned Spacecraft
Center like when you first arrived there? Essentially it was really
a new center altogether.
Shea: It wasn't on the base yet. I went
down and I just immersed myself into the organization, not as a headquarters
guy, but as one of their guys. I was really Mueller's guy in Houston,
but I acted as if Mueller was headquarters just like anybody else,
and became part of the center. I assigned studies to various parts
of the organization that I thought would cause them to change their
mind about the things that were wrong, that were wrong, in my mind.
Kelly: Can you tell me about some of
the people that you worked with when you were out there?
Shea: Tom [J. Thomas] Markley, the guy
who just called, he became my deputy. He was a very strong guy, a
very strong guy. Faget was there, of course.
I didn't tell you the story about when I went around to start the
studies on LOR direct flight. I went to von Braun. I had no organization
in Washington. I had maybe two people. I said I needed some people,
and he gave me one guy, named Arthur Rudolph, an old guy who used
to run the factory at Peenemunde. I went to Gilruth, he turned me
over to Faget. Faget said to me, in Faget's gracious way, "You're
not getting anybody from me. I have a thousand people, you have hardly
anybody. We're ahead of you, we'll always stay ahead of you. We don't
need you, you get nothing."
Then I went out to JPL [Jet Propulsion Laboratory] and talked to Bill
[William H.] Pickering, who's a moralist, you know, and Pickering
said, "Of course you have a problem." And Pickering assigned
thirteen of his better people to Washington, detailed to Washington
for six months, and they were the ones that actually did the back
work on writing the reports and so on. Not Manned Space Flight people,
but JPL people.
Kelly: It seems like he really helped
you out.
Shea: Oh, he did, yes.
Kelly: What then did those people go
on to do?
Shea: Well, they went back. One was
Ed Recatin, who became president of Aerospace Corporation. [Later,]
he was director of DARPA, the Defense [Advanced] Research Projects
Agency. They were good guys.
Kelly: That's terrific. Any other people
of note that you might want to mention, people you worked with at
the Manned Spacecraft Center?
Shea: Well, a guy named Rolph [W.] Lanzkron,
L-A-N-Z-K-R-O-N. That's all part of the story of what went on down
there. If you choose to come back again, we'll get into that.
Kelly: I would love to do that if you
would be willing to do that.
Shea: I don't know if this is useful
for you or not.
Kelly: Oh, absolutely. This is marvelous.
Kelly: As a matter of fact, as I mentioned,
what we're trying to do is just trying to get a very broad overview
of what happened with Mercury through Apollo Programs, and this fits
right into the very beginning of Apollo.
Shea: This is a very negative view,
but it's a very true view.
Kelly: That's what we're looking for.
We're looking for history and documenting history, and these are the
actual documents.
Shea: Some of them are the actual documents.
Kelly: That is going to be really terrific
research. Is there anything you would like to talk about today?
Shea: I think we've pretty well covered
… the system engineering part of it. I'm still writing more
stuff. I have a secretary that's typing for me. Maybe when you come
back again, I'll have a few more things for you.
Kelly: That sounds terrific. What I'd
like to propose, if this is okay for you, I'd like to read through
this research, and listen to this tape a little bit more, and go through
it a little bit more in depth, and do some more research on my own—
Shea: And come back again.
Kelly: —and come back with more
detailed questions.
Shea: Certainly. I'm retired. There's
not restriction on my time. If it's useful for you.
Kelly: Absolutely.
Shea: The only thing I would say is
I consider some of the material proprietary.
Kelly: I understand. Certainly.
Shea: The stories are, like that story
there, perfectly permissible to talk about.
[End
of interview]