HiBEX ABM

Found this on the CIA FOIA site:

April 20, 1962

MEMORANDUM FOR: Dr. Jerome B. Wiesner
FROM: AICBM Panel
SUBJECT: NIKE ZEUS and Hard Point Defense

The Panel discussed the future of the NIKE ZEUS program with representatives of DDR&E and the Army, the Air Force and WSEG. Some general comments arising from these discussions are the following:

(1) Hard point AICBM defense of command and control centers of high value appears to us to offer an important defense element. If the presently envisaged performance of "sprint" anti-missiles and ZMAR radars can be achieved, such defenses seem feasible and attractive. We have not attempted to compare the economics of active defense with other measures such as extreme hardening, redundancy, or mobility.

(2) DDR&E is considering a reoriented NIKE ZEUS system which would intercept incoming ICBM's at much lower altitude and would thus permit atmospheric decoy discrimination. In order to do this, they propose to raise substantially the standards for acceptable damage to a city. Overpressure of as much as 15 psi and thermal flux as high as 100 calories per square centimeter is suggested as possible "last-ditch" damage criteria. This approach would appear to only make sense in combination with a city blast shelter program. In this respect, these studies try to identify the hard point defense and the city defense problem by re-defining cities as a hard target.

(3) Consideration of hard point AICBM defense of hardened ICBM sites indicates that this is only worth considering if the survival probability of the hardened site per se is small and the cost per anti-missile is low. Most of the anti-missile systems do not meet this requirement.

(4) We believe that the potential usefulness of an advanced hard point AICBM system is sufficient to justify immediate commencement of R&D on it. This is especially true since there are important unsolved design problems in the development of a sprint missile, such as heating of the case and the possibility of structural failure of the propellant and other elements. One of the main difficulties with the AICBM program in the past has been that deployment of a system was always so far in the future that the usefulness of the system by that time was very questionable.

(5) We recommend, therefore, that there be much more vigorous pursuit of the R&D program for a hard point AICBM system with particular emphasis on the development of a high performance (sprint) anti-missile missile. It will be important to keep the requirements on performance, especially of the radar, sufficiently modest to permit rapid development. This will probably mean focusing on one application rather than demanding applicability for several purposes. We, therefore, recommend that command and control centers be considered the priority application of hard point AICBM defense rather than "hard city" defense.

This seems to contain the design parameters for HIBEX; 15 PSI + 100 cal/cm2.
 
https://apps.dtic.mil/sti/tr/pdf/AD0915422.pdf
The Data Processing/HAPDAR Field Test Facility was created by adding anIBM 360/63 Computer and specially developed software to the existing SperryRand HAPDAR (Hardpoint Demonstration Array Radar) at White Sands MissileRange, New Mexico
 
From

ODDR&E
ASSESSMENT
OF
BALLISTIC MISSILE DEFENSE PROGRAM

17 April 1961

PPD 61-33

DEFENSE OF HARD POINTS

Defense of the United States retaliatory force (including command and control centers) against ICBM attack can be accomplished to some degree by: increasing numbers, hardening, concealment, and active defense.

A plausible case can be made to show that hardening plus active defense offers economic and reliability advantages over the other alternatives for some important elements of the United States retaliatory arsenal. This claim must be tempered, however, by an appreciation of technological uncertainties which prevent a positive statement at this date that active defense of hard points is technically feasible at a level of deployment which makes it economically attractive.

Hard point defense is, beyond much question, easier and less expensive to accomplish than defense of soft areas. Since the target is hard, the incoming missile may be allowed to come within about ten thousand feet of its target prior to interception. In consequence, commitment of the AICBM weapon may be delayed until the ICBM is within ten-to-twenty miles of the target, rather than the sixty-to-one hundred miles minimum commitment range for ZEUS, for example. This results in less expensive interceptors and very likely reduces the cost of other system elements as well. The decoy problem is also eased, as decoys to be effective must be capable of surviving the most rigorous re-entry problems without disclosing their characteristics to observing radars, and must have been precisely deployed in order to appear to impact within ten thousand feet of the target.

The Air Force has recently concluded eight studies (six unfunded, two funded, for a total of $140,000) of the means of defending a hardened restricted area against ballistic missile attack. The RAND Corporation and Bell Telephone Laboratories have also recently concluded similar studies. These studies indicate that reasonably good defense of small sites hardened to about 100 psi can be bought at a five-year cost in the range of ten-to-fifty million dollars, depending upon the severity of the postulated threat.

While it seems quite likely that a hard point defense system costing fifty million per defended site or somewhat less could be built with the capability of handling perhaps ten decoys per missile attack, the costs would rise almost linearly with increasing numbers of re-entry decoys. As of now it is not known whether it is possible to perfect decoys which weigh a few tens of pounds or less, and which can survive re-entry while matching medium or large warheads in CEP and characteristics observable by radar.

Until this crucial uncertainty is resolved, the feasibility of hard point defense at reasonable cost cannot be determined.

A technically different approach to hard point defense (for example, HELMET) is being given some consideration. Rather than employing anti-missiles which seek out incoming missiles and are therefore vulnerable to decoying, these concepts involve lofting a barrage of pellets through which dangerous objects would have to fly. Warhead and decoy alike would be destroyed if the barrier were sufficiently high (so that atmospheric slowdown had not occurred) and the pellets of the barrage sufficiently heavy to accomplish kill. Considering the uncertainty of our current knowledge, the weight of pellets required may range from one million to one hundred million pounds per attack for each hard target defended. Systems of this kind have not yet been examined closely enough to determine their cost or susceptibility to specific countermeasures.

Another significant uncertainty relates to the feasibility of countering the effects on defense systems of large, low-altitude, nuclear bursts; or alternatively, the possibility of successfully attacking with weapons which deny the possibility of the enemy's warheads detonating.

The Penetration Aids program as well as the decoy discrimination research carried on in ZEUS and DEFENDER will go a long way toward resolving the uncertainties in decoy capability. Resolving the questions raised by possible nuclear detonations is not possible without testing; but theoretical studies based on available data may furnish a useful degree of knowledge.

The Air Force has estimated that about [REDACTED] would be required between the start of weapon system development and IOC. Some research in hard point defense technology is being conducted at present, and some of the system problems are closely related to those experienced in ZEUS and ARPAT. Increasing the effort on technology related to hard point defense (especially work on high thrust, short-burning time interceptors) is desirable at this time. Some limited systems work should be undertaken to pin down costs and prepare for possible weapon system development.
 
REPORT OF THE DEFENSE SCIENCE BOARD
February 1967
Report of the Task Group on Independent Research and Development

TITLE: Boeing HIBEX IR&D Effort

BRIEF DESCRIPTION:

IR&D research was implemented in 1960 in the area of high-acceleration boosters, to satisfy requirements of an anti-ballistic missile. Specific IR&D effort undertaken included advanced defense techniques, high-acceleration propulsion, fast-response maneuverability and control during boost phase, hot launch of a missile with closed breech, and the survival of electrical and mechanical equipment in a very high-acceleration and high-dynamic-pressure environment. This research led to a contract, DA-01-021-AMC-10696(Z), under the direction of ARPA.

Program effort required approximately $450,000 in Boeing IR&D funds. The HIBEX contract value was $22,000,000.

Significant IR&D documentation includes: D2-35005, Hardsite/Urban Defense Missile Six Week Study Report; D2-35007, Spring Technical Task Description; D2-22294, Plasma Research - Hard Point Missile; D2-35010, Preliminary Description - Combo Terminal AICBM Interceptor; D2-20864, Hard Point AICBM Studies - Supplementary Technical Data; D2-22676, HIBEX Design Data; D2-22557, High-g Boost Experiment Oral Presentation; D2-20228, Hard Point Defense Interceptor (HFDI) Experiment Technical and Management Proposal.

BENEFITS TO THE DOD RESULTING FROM THE EFFORT:

The HIBEX program and associated research have provided a significant increase in the demonstrated high-acceleration booster technology and have validated the feasibility of very high-acceleration intercepts. Further, it has been demonstrated that a system with fast reaction time can be developed with low-altitude commitment which greatly simplifies radar requirements. The results of this have not yet been incorporated in a defense system, but the technology developed should form a significant building block for future systems.
 
From

ODDR&E
ASSESSMENT
OF
BALLISTIC MISSILE DEFENSE PROGRAM

17 April 1961

PPD 61-33
"One million to one hundred million lbs of pellets to stop an attack on a single hard target." Say what?
 
HAPDAR could only track 5 simultaneous targets at a time; due to limitations of the 1218 computer at the site.

Source:
IEEE 1966 Aerospace and Electronic Systems Convention Record
 

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